<?xml version="1.0" encoding="utf-8"?><rss version="2.0"><channel><title>RSS for J AEROSP ENG</title><link>http://academic.research.microsoft.com/Rss.aspx?id=5477&amp;cata=6</link><description>Search RSS feed for Microsoft Academic Search</description><generator>MSRA Libra RSS Burner</generator><copyright>(c)2008 Microsoft Corpration, All right reserved.</copyright><pubDate>Mon, 20 May 2013 14:32:11 GMT</pubDate><lastBuildDate>Mon, 20 May 2013 14:32:11 GMT</lastBuildDate><category /><item><title>Geotechnical Properties of JSC1A Lunar Soil Simulant</title><link>http://academic.research.microsoft.com/Publication/26912649</link><pubDate>Mon, 20 May 2013 14:32:11 GMT</pubDate><guid isPermaLink="false">26912649</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/53662925">Xiangwu Zeng</a>, <a href="http://academic.research.microsoft.com/Author/22237878">Chunmei He</a>, <a href="http://academic.research.microsoft.com/Author/22237879">Heather Oravec</a>, <a href="http://academic.research.microsoft.com/Author/22225964">Allen Wilkinson</a>, <a href="http://academic.research.microsoft.com/Author/42507486">Juan Agui</a>, <a href="http://academic.research.microsoft.com/Author/49315524">Vivake Asnani</a><span style="margin-left:20px">(Citations:5)</span><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v23/i2/p111/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 23, no. 2, 2010</cite>]]></description></item><item><title>Engineering Properties of Lunar Soil Simulant JSC1A</title><link>http://academic.research.microsoft.com/Publication/26912665</link><pubDate>Mon, 20 May 2013 14:32:10 GMT</pubDate><guid isPermaLink="false">26912665</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/19091284">Haydar Arslan</a>, <a href="http://academic.research.microsoft.com/Author/52411657">Susan Batiste</a>, <a href="http://academic.research.microsoft.com/Author/18256771">Stein Sture</a><span style="margin-left:20px">(Citations:4)</span><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v23/i1/p70/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 23, no. 1, 2010</cite>]]></description></item><item><title>Effect of Concrete Substrate Repair Methods for Beams Aged by Accelerated Corrosion and Strengthened with CFRP</title><link>http://academic.research.microsoft.com/Publication/26912685</link><pubDate>Mon, 20 May 2013 14:32:09 GMT</pubDate><guid isPermaLink="false">26912685</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/96295">Indrajit Ray</a>, <a href="http://academic.research.microsoft.com/Author/22237904">George C. Parish</a>, <a href="http://academic.research.microsoft.com/Author/3736335">Julio F. Davalos</a>, <a href="http://academic.research.microsoft.com/Author/9313325">An Chen</a><span style="margin-left:20px">(Citations:2)</span><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000030">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Boundary Layer Effect in Composite Beams with Interlayer Slip</title><link>http://academic.research.microsoft.com/Publication/26912694</link><pubDate>Mon, 20 May 2013 14:32:08 GMT</pubDate><guid isPermaLink="false">26912694</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/13357002">Noël Challamel</a>, <a href="http://academic.research.microsoft.com/Author/21837428">Ulf Arne Girhammar</a><span style="margin-left:20px">(Citations:3)</span><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000027">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Vision-Based Indoor Localization for Unmanned Aerial Vehicles</title><link>http://academic.research.microsoft.com/Publication/26912672</link><pubDate>Mon, 20 May 2013 14:32:07 GMT</pubDate><guid isPermaLink="false">26912672</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/446263">Jeong-Oog Lee</a>, <a href="http://academic.research.microsoft.com/Author/12679038">Taesam Kang</a>, <a href="http://academic.research.microsoft.com/Author/22237897">Keun-Hwan Lee</a>, <a href="http://academic.research.microsoft.com/Author/22237898">Sung Kyu Im</a><span style="margin-left:20px">(Citations:1)</span><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000064">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Planform and Flexibility on Lift Characteristics for Flow over Low-Aspect Ratio Wings</title><link>http://academic.research.microsoft.com/Publication/26912664</link><pubDate>Mon, 20 May 2013 14:32:06 GMT</pubDate><guid isPermaLink="false">26912664</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/22237891">L. 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Ferrero</a><span style="margin-left:20px">(Citations:1)</span><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000061">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Stochastic Free Vibration Response of Soft Core Sandwich Plates Using an Improved Higher-Order Zigzag Theory</title><link>http://academic.research.microsoft.com/Publication/26912658</link><pubDate>Mon, 20 May 2013 14:32:03 GMT</pubDate><guid isPermaLink="false">26912658</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/23114747">Mihir K. Pandit</a>, <a href="http://academic.research.microsoft.com/Author/47177723">Bhrigu N. Singh</a>, <a href="http://academic.research.microsoft.com/Author/18174164">Abdul H. 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Alshibli</a><span style="margin-left:20px">(Citations:1)</span><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000020">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Flutter Control of Smart Composite Structures in Hygrothermal Environment</title><link>http://academic.research.microsoft.com/Publication/26912684</link><pubDate>Mon, 20 May 2013 14:31:57 GMT</pubDate><guid isPermaLink="false">26912684</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/21978910">P. K. Mahato</a>, <a href="http://academic.research.microsoft.com/Author/21708668">D. K. Maiti</a><span style="margin-left:20px">(Citations:1)</span><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000046">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Structural Uncertainity Effect on Classical Wing Flutter Characteristics</title><link>http://academic.research.microsoft.com/Publication/26912682</link><pubDate>Mon, 20 May 2013 14:31:56 GMT</pubDate><guid isPermaLink="false">26912682</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/3739323">F. Borello</a>, <a href="http://academic.research.microsoft.com/Author/4853258">E. Cestino</a>, <a href="http://academic.research.microsoft.com/Author/2911742">G. Frulla</a><span style="margin-left:20px">(Citations:1)</span><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000049">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Nonlinear Fracture Analysis of Delamination Crack Jumps in Laminated Composites</title><link>http://academic.research.microsoft.com/Publication/26912667</link><pubDate>Mon, 20 May 2013 14:31:55 GMT</pubDate><guid isPermaLink="false">26912667</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/22225994">D. S. Ling</a>, <a href="http://academic.research.microsoft.com/Author/22119080">X. J. Fang</a>, <a href="http://academic.research.microsoft.com/Author/13027277">B. N. Cox</a>, <a href="http://academic.research.microsoft.com/Author/53644424">Q. D. Yang</a><span style="margin-left:20px">(Citations:1)</span><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000032">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>A Stochastic Six-Degree-of-Freedom Flight Simulator for Passively Controlled High Power Rockets</title><link>http://academic.research.microsoft.com/Publication/26912689</link><pubDate>Mon, 20 May 2013 14:31:54 GMT</pubDate><guid isPermaLink="false">26912689</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/53298702">Simon Box</a>, <a href="http://academic.research.microsoft.com/Author/719294">Christopher M. 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Taeibi-Rahni</a>, <a href="http://academic.research.microsoft.com/Author/22237885">F. Sabetghadam</a>, <a href="http://academic.research.microsoft.com/Author/22237886">M. K. Moayyedi</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v23/i1/p44/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 23, no. 1, 2010</cite>]]></description></item><item><title>Robust MIMO H∞ Integral-Backstepping PID Controller for Hovering Control of Unmanned Model Helicopter</title><link>http://academic.research.microsoft.com/Publication/26912693</link><pubDate>Mon, 20 May 2013 14:31:51 GMT</pubDate><guid isPermaLink="false">26912693</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/22237908">Wisnu Adi Pradana</a>, <a href="http://academic.research.microsoft.com/Author/18166296">Endra Joelianto</a>, <a href="http://academic.research.microsoft.com/Author/2698324">Agus Budiyono</a>, <a href="http://academic.research.microsoft.com/Author/3666169">Widyawardana Adiprawita</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000074">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Numerical∕Experimental Correlation of a Plasma Wind Tunnel Test on an UHTC Made Nose Cap of a Re-Entry Vehicle</title><link>http://academic.research.microsoft.com/Publication/26912683</link><pubDate>Mon, 20 May 2013 14:31:50 GMT</pubDate><guid isPermaLink="false">26912683</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/21990352">Rosario Borrelli</a>, <a href="http://academic.research.microsoft.com/Author/52938196">Aniello Riccio</a>, <a href="http://academic.research.microsoft.com/Author/21990354">Domenico Tescione</a>, <a href="http://academic.research.microsoft.com/Author/21989176">Roberto Gardi</a>, <a href="http://academic.research.microsoft.com/Author/53618576">Giuliano Marino</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000047">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>An Engineering Method for Air-Cooling Design of 2Seat Propeller Driven Aircraft Powered by Fuel Cells</title><link>http://academic.research.microsoft.com/Publication/26912686</link><pubDate>Mon, 20 May 2013 14:31:49 GMT</pubDate><guid isPermaLink="false">26912686</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/23123457">G. Romeo</a>, <a href="http://academic.research.microsoft.com/Author/4853258">E. Cestino</a>, <a href="http://academic.research.microsoft.com/Author/3739323">F. Borello</a>, <a href="http://academic.research.microsoft.com/Author/22022526">G. Correa</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000055">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Analysis of a Lunar Base Structure Using the Discrete Element Method</title><link>http://academic.research.microsoft.com/Publication/26912692</link><pubDate>Mon, 20 May 2013 14:31:48 GMT</pubDate><guid isPermaLink="false">26912692</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/22837561">Axel R. Tóth</a>, <a href="http://academic.research.microsoft.com/Author/18089793">Katalin Bagi</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000073">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Identification and Monitoring of Modal Parameters in Aircraft Structures Using the Natural Excitation Technique (NExT) Combined with the Eigensystem Realization Algorithm (ERA)</title><link>http://academic.research.microsoft.com/Publication/26912647</link><pubDate>Mon, 20 May 2013 14:31:47 GMT</pubDate><guid isPermaLink="false">26912647</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/22237876">Hever Moncayo</a>, <a href="http://academic.research.microsoft.com/Author/22237877">Johannio Marulanda</a>, <a href="http://academic.research.microsoft.com/Author/1121692">Peter Thomson</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v23/i2/p99/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 23, no. 2, 2010</cite>]]></description></item><item><title>Series Solution of Wire Coating Analysis Involving MHD Johnson-Segalman Fluid</title><link>http://academic.research.microsoft.com/Publication/26912661</link><pubDate>Mon, 20 May 2013 14:31:46 GMT</pubDate><guid isPermaLink="false">26912661</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/3679676">M. Sajid</a>, <a href="http://academic.research.microsoft.com/Author/12958616">T. Hayat</a>, <a href="http://academic.research.microsoft.com/Author/12961588">S. Asghar</a>, <a href="http://academic.research.microsoft.com/Author/12961589">A. M. Siddiqui</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v23/i1/p84/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 23, no. 1, 2010</cite>]]></description></item><item><title>Preimpact Configuration Analysis of Dual-Arm Space Manipulator Capturing Object</title><link>http://academic.research.microsoft.com/Publication/26912644</link><pubDate>Mon, 20 May 2013 14:31:45 GMT</pubDate><guid isPermaLink="false">26912644</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/22237871">P. C. Cong</a>, <a href="http://academic.research.microsoft.com/Author/54041701">Z. W. Sun</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v23/i2/p117/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 23, no. 2, 2010</cite>]]></description></item><item><title>Improvement of the Parameterised Identification Model Using Quasi-steady and Non-Uniform Inflow Aerodynamic Model</title><link>http://academic.research.microsoft.com/Publication/26912671</link><pubDate>Mon, 20 May 2013 14:31:44 GMT</pubDate><guid isPermaLink="false">26912671</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/22483760">Vaitla Laxman</a>, <a href="http://academic.research.microsoft.com/Author/2698324">Agus Budiyono</a>, <a href="http://academic.research.microsoft.com/Author/13530432">Kwang Joon Yoon</a>, <a href="http://academic.research.microsoft.com/Author/46756953">Yung Hwan Byun</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000065">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Thermal Scale Modeling by FEM and Test</title><link>http://academic.research.microsoft.com/Publication/26912666</link><pubDate>Mon, 20 May 2013 14:31:43 GMT</pubDate><guid isPermaLink="false">26912666</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/52297355">M. H. Sabour</a>, <a href="http://academic.research.microsoft.com/Author/39612415">R. B. Bhat</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v23/i1/p24/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 23, no. 1, 2010</cite>]]></description></item><item><title>Robust Dynamic Sliding Mode Control of a Rotating Thin-Walled Composite Blade</title><link>http://academic.research.microsoft.com/Publication/26912691</link><pubDate>Mon, 20 May 2013 14:31:42 GMT</pubDate><guid isPermaLink="false">26912691</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/21727427">Sungsoo Na</a>, <a href="http://academic.research.microsoft.com/Author/21807464">Bokhee Lee</a>, <a href="http://academic.research.microsoft.com/Author/21807465">Jeonghwan Choo</a>, <a href="http://academic.research.microsoft.com/Author/6178823">Piergiovanni Marzocca</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000076">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Z-Pin Composites: Aerospace Structural Design Considerations</title><link>http://academic.research.microsoft.com/Publication/26912695</link><pubDate>Mon, 20 May 2013 14:31:41 GMT</pubDate><guid isPermaLink="false">26912695</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/18156804">A. P. Mouritz</a>, <a href="http://academic.research.microsoft.com/Author/10508143">P. Chang</a>, <a href="http://academic.research.microsoft.com/Author/18995501">M. D. Isa</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000078">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Finite Element Model for Failure Study of Two Dimensional Triaxially Braided Composite</title><link>http://academic.research.microsoft.com/Publication/26912653</link><pubDate>Mon, 20 May 2013 14:31:40 GMT</pubDate><guid isPermaLink="false">26912653</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/43228303">Xuetao Li</a>, <a href="http://academic.research.microsoft.com/Author/7873767">Wieslaw K. Binienda</a>, <a href="http://academic.research.microsoft.com/Author/18474048">Robert K. Goldberg</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000029">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Practical Assessment of Real-Time Impact Point Estimators for Smart Weapons</title><link>http://academic.research.microsoft.com/Publication/26912681</link><pubDate>Mon, 20 May 2013 14:31:39 GMT</pubDate><guid isPermaLink="false">26912681</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/5169919">Frank Fresconi</a>, <a href="http://academic.research.microsoft.com/Author/22492375">Gene Cooper</a>, <a href="http://academic.research.microsoft.com/Author/49218773">Mark Costello</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000044">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Magnetic Space Launcher</title><link>http://academic.research.microsoft.com/Publication/26912651</link><pubDate>Mon, 20 May 2013 14:31:38 GMT</pubDate><guid isPermaLink="false">26912651</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/13239506">Alexander Bolonkin</a>, <a href="http://academic.research.microsoft.com/Author/51492500">Mark Krinker</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://arxiv.org/abs/0903.5008">view publication</a></span></p><p>A method and facilities for delivering payload and people into outer space are presented. This method uses, in general, engines located on a planetary surface. The installation consists of a space apparatus, power drive stations, which include a flywheel accumulator (for storage) of energy, a variable reducer, a powerful homopolar electric generator and electric rails. The drive stations accelerate the ...</p><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Some Comments on the Protection of Lunar Habitats against Damage from Meteoroid Impacts</title><link>http://academic.research.microsoft.com/Publication/26912660</link><pubDate>Mon, 20 May 2013 14:31:37 GMT</pubDate><guid isPermaLink="false">26912660</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/21726711">W. P. Schonberg</a>, <a href="http://academic.research.microsoft.com/Author/55541912">F. Schäfer</a>, <a href="http://academic.research.microsoft.com/Author/21968459">R. Putzar</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v23/i1/p90/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 23, no. 1, 2010</cite>]]></description></item><item><title>Railgun Space Launcher</title><link>http://academic.research.microsoft.com/Publication/26912677</link><pubDate>Mon, 20 May 2013 14:31:36 GMT</pubDate><guid isPermaLink="false">26912677</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/13239506">Alexander Bolonkin</a>, <a href="http://academic.research.microsoft.com/Author/51492500">Mark Krinker</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000041">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Lunar Habitat Micrometeoroid and Radiation Shielding: Options, Applications and Assessments</title><link>http://academic.research.microsoft.com/Publication/26912687</link><pubDate>Mon, 20 May 2013 14:31:35 GMT</pubDate><guid isPermaLink="false">26912687</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/43983692">Larry Bell</a>, <a href="http://academic.research.microsoft.com/Author/21990898">Olga Bannova</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000054">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Robust Nonlinear Optimal Solution to the Lunar Landing Guidance by Using Neighboring Optimal Control</title><link>http://academic.research.microsoft.com/Publication/26912680</link><pubDate>Mon, 20 May 2013 14:31:34 GMT</pubDate><guid isPermaLink="false">26912680</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/13528907">Hamed Hossein Afshari</a>, <a href="http://academic.research.microsoft.com/Author/13528909">Jafar Roshanian</a>, <a href="http://academic.research.microsoft.com/Author/13528908">Alireza Novinzadeh</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000048">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Fuzzy Active Control of Flexible Structures by Using Electromagnetic Actuators</title><link>http://academic.research.microsoft.com/Publication/26912668</link><pubDate>Mon, 20 May 2013 14:31:33 GMT</pubDate><guid isPermaLink="false">26912668</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/21968027">Jarir Mahfoud</a>, <a href="http://academic.research.microsoft.com/Author/41902985">Johan Der Hagopian</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000067">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Design and Analysis of a Wind-Driven Spherical Robot with Multiple Shapes for Environment Exploration</title><link>http://academic.research.microsoft.com/Publication/26912656</link><pubDate>Mon, 20 May 2013 14:31:32 GMT</pubDate><guid isPermaLink="false">26912656</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/53556897">Tuanjie Li</a>, <a href="http://academic.research.microsoft.com/Author/22237883">Weigang Liu</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000063">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Fault Tolerant Attitude Synchronization Control during Formation Flying</title><link>http://academic.research.microsoft.com/Publication/26912697</link><pubDate>Mon, 20 May 2013 14:31:31 GMT</pubDate><guid isPermaLink="false">26912697</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/3524921">Junquan Li</a>, <a href="http://academic.research.microsoft.com/Author/53462508">Krishna Dev Kumar</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000080">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Free Vibration Analysis of Cylindrical Shells Supported on Parts of the Edges</title><link>http://academic.research.microsoft.com/Publication/26912663</link><pubDate>Mon, 20 May 2013 14:31:30 GMT</pubDate><guid isPermaLink="false">26912663</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/3632731">S. Kandasamy</a>, <a href="http://academic.research.microsoft.com/Author/53657947">A. V. Singh</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v23/i1/p34/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 23, no. 1, 2010</cite>]]></description></item><item><title>Error Analysis and Cycle-Slip Detection Research on Satellite-Borne GPS Observation</title><link>http://academic.research.microsoft.com/Publication/26912654</link><pubDate>Mon, 20 May 2013 14:31:29 GMT</pubDate><guid isPermaLink="false">26912654</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/47569213">Y. Miao</a>, <a href="http://academic.research.microsoft.com/Author/54041701">Z. W. Sun</a>, <a href="http://academic.research.microsoft.com/Author/3362185">S. N. Wu</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000056">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Indirect Flight Control System Properties Shaping for General Aviation Aircraft</title><link>http://academic.research.microsoft.com/Publication/26912688</link><pubDate>Mon, 20 May 2013 14:31:28 GMT</pubDate><guid isPermaLink="false">26912688</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/21842846">Andrzej Tomczyk</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000053">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Accelerometer Based Force Balance for High Enthalpy Facilities</title><link>http://academic.research.microsoft.com/Publication/26912675</link><pubDate>Mon, 20 May 2013 14:31:27 GMT</pubDate><guid isPermaLink="false">26912675</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/41993794">Vinayak Kulkarni</a>, <a href="http://academic.research.microsoft.com/Author/12711500">K. P. J. Reddy</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000040">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Magnetic Suspended AB-Structures and Motionless Space Stations</title><link>http://academic.research.microsoft.com/Publication/26912652</link><pubDate>Mon, 20 May 2013 14:31:26 GMT</pubDate><guid isPermaLink="false">26912652</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/13239506">Alexander Bolonkin</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000058">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Femtotechnology: Design of the Strongest AB-Matter for Aerospace</title><link>http://academic.research.microsoft.com/Publication/26912679</link><pubDate>Mon, 20 May 2013 14:31:25 GMT</pubDate><guid isPermaLink="false">26912679</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/13239506">A. A. Bolonkin</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000042">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Adaptive Output Feedback Control of Spacecraft Formation Flying Using Chebyshev Neural Networks</title><link>http://academic.research.microsoft.com/Publication/26912690</link><pubDate>Mon, 20 May 2013 14:31:24 GMT</pubDate><guid isPermaLink="false">26912690</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/3525219">An-Min Zou</a>, <a href="http://academic.research.microsoft.com/Author/53462508">K. D. Kumar</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000072">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Crack Growth Resistance of Hybrid Fiber Reinforced Cement Matrix Composites</title><link>http://academic.research.microsoft.com/Publication/26912673</link><pubDate>Mon, 20 May 2013 14:31:23 GMT</pubDate><guid isPermaLink="false">26912673</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/620176">Ying Chen</a>, <a href="http://academic.research.microsoft.com/Author/3676251">Pizhong Qiao</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000031">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Periodical Motion of Tethered Satellite System around Collinear Libration Points</title><link>http://academic.research.microsoft.com/Publication/26912696</link><pubDate>Mon, 20 May 2013 14:31:22 GMT</pubDate><guid isPermaLink="false">26912696</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/27522691">Rui Zhong</a>, <a href="http://academic.research.microsoft.com/Author/21772230">Shijie Xu</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000077">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Nonlinear Controller Synthesis for Single-Input Multiple-Output Systems with Application to Cruise Missile</title><link>http://academic.research.microsoft.com/Publication/26912648</link><pubDate>Mon, 20 May 2013 14:31:21 GMT</pubDate><guid isPermaLink="false">26912648</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/18194027">Amir Nassirharand</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v23/i2/p105/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 23, no. 2, 2010</cite>]]></description></item><item><title>On the Motion of a Rigid Body in a Newtonian Field of Force Exerted by Three Attracting Centers</title><link>http://academic.research.microsoft.com/Publication/26912670</link><pubDate>Mon, 20 May 2013 14:31:20 GMT</pubDate><guid isPermaLink="false">26912670</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/54206296">A. I. Ismail</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000069">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Dynamic Model of an Astronaut Equipped with a Manned Maneuvering Unit in Virtual Reality</title><link>http://academic.research.microsoft.com/Publication/26912643</link><pubDate>Mon, 20 May 2013 14:31:19 GMT</pubDate><guid isPermaLink="false">26912643</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/254663">Cheng Jian</a>, <a href="http://academic.research.microsoft.com/Author/21722708">Fan Xiumin</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v23/i2/p139/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 23, no. 2, 2010</cite>]]></description></item><item><title>Ballistic Walking Design via Impulsive Control</title><link>http://academic.research.microsoft.com/Publication/26912645</link><pubDate>Mon, 20 May 2013 14:31:18 GMT</pubDate><guid isPermaLink="false">26912645</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/24469651">Alexander M. Formal’skii</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v23/i2/p129/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 23, no. 2, 2010</cite>]]></description></item><item><title>Top-Level Considerations for Planning Lunar/Planetary Habitat Structures</title><link>http://academic.research.microsoft.com/Publication/26912655</link><pubDate>Mon, 20 May 2013 14:31:17 GMT</pubDate><guid isPermaLink="false">26912655</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/43983692">Larry Bell</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000062">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Relative Circular Navigation Guidance for Three Dimensional Impact Angle Control Problem</title><link>http://academic.research.microsoft.com/Publication/26912676</link><pubDate>Mon, 20 May 2013 14:31:16 GMT</pubDate><guid isPermaLink="false">26912676</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/34127573">Myung-Gon Yoon</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000043">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2010</cite>]]></description></item><item><title>Jet-Induced Cratering of a Granular Surface with Application to Lunar Spaceports</title><link>http://academic.research.microsoft.com/Publication/26912589</link><pubDate>Mon, 20 May 2013 14:31:15 GMT</pubDate><guid isPermaLink="false">26912589</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/48249529">Philip T. Metzger</a>, <a href="http://academic.research.microsoft.com/Author/22237832">Christopher D. Immer</a>, <a href="http://academic.research.microsoft.com/Author/22237833">Carly M. Donahue</a>, <a href="http://academic.research.microsoft.com/Author/48710271">Bruce T. Vu</a>, <a href="http://academic.research.microsoft.com/Author/22237835">Robert C. Latta III</a>, <a href="http://academic.research.microsoft.com/Author/22237836">Matthew Deyo-Svendsen</a><span style="margin-left:20px">(Citations:4)</span><span style="margin-left:20px"><a href="http://arxiv.org/abs/0906.0196">view publication</a></span></p><p>The erosion of lunar soil by rocket exhaust plumes is investigated experimentally. This has identified the diffusion-driven flow in the bulk of the sand as an important but previously unrecognized mechanism for erosion dynamics. It has also shown that slow regime cratering is governed by the recirculation of sand in the widening geometry of the crater. Scaling relationships and ...</p><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 1, 2009</cite>]]></description></item><item><title>Development of Fabric Constitutive Behavior for Use in Modeling Engine Fan Blade-Out Events</title><link>http://academic.research.microsoft.com/Publication/6152703</link><pubDate>Mon, 20 May 2013 14:31:14 GMT</pubDate><guid isPermaLink="false">6152703</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/1140384">S. Bansal</a>, <a href="http://academic.research.microsoft.com/Author/12668445">B. Mobasher</a>, <a href="http://academic.research.microsoft.com/Author/48089998">S. D. Rajan</a>, <a href="http://academic.research.microsoft.com/Author/5264362">I. Vintilescu</a><span style="margin-left:20px">(Citations:3)</span><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i3/p249/s1&Agg=doi">view publication</a></span></p><p>The development of a robust and reliable material model for fabrics used to prevent fan blade-out events in propulsion engines has significant importance in the design of fan-containment systems. Currently, Kevlar is the only fabric approved by the Federal Aviation Administration to be used in fan-containment systems. However, very little work has been done in building a ...</p><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 3, 2009</cite>]]></description></item><item><title>3D Shape Characterization and Image-Based DEM Simulation of the Lunar Soil Simulant FJS-1</title><link>http://academic.research.microsoft.com/Publication/10795541</link><pubDate>Mon, 20 May 2013 14:31:13 GMT</pubDate><guid isPermaLink="false">10795541</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/54983799">Takashi Matsushima</a>, <a href="http://academic.research.microsoft.com/Author/54632446">Jun Katagiri</a>, <a href="http://academic.research.microsoft.com/Author/41870487">Kentaro Uesugi</a>, <a href="http://academic.research.microsoft.com/Author/51959497">Akira Tsuchiyama</a>, <a href="http://academic.research.microsoft.com/Author/52494480">Tsukaka Nakano</a><span style="margin-left:20px">(Citations:5)</span><span style="margin-left:20px"><a href="http://granular.kz.tsukuba.ac.jp/dem/cr01/200901_jae.pdf">view publication</a></span></p><p>This paper describes a procedure used to characterize the three-dimensional 3D grain shape of lunar soil and undertake simulations of lunar soil by image-based discrete element method DEM. Given that detailed 3D grain-shape information is unavailable for real lunar soil, a simulant material, FJS-1, is used in this study. We use the high-resolution micro X-...</p><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 1, 2009</cite>]]></description></item><item><title>Application of Optical Measurement Techniques to Supersonic and Hypersonic Aerospace Flows</title><link>http://academic.research.microsoft.com/Publication/26912626</link><pubDate>Mon, 20 May 2013 14:31:12 GMT</pubDate><guid isPermaLink="false">26912626</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/22237864">David Estruch</a>, <a href="http://academic.research.microsoft.com/Author/18168614">Nicholas J. Lawson</a>, <a href="http://academic.research.microsoft.com/Author/54753914">Kevin P. Garry</a><span style="margin-left:20px">(Citations:2)</span><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i4/p383/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 4, 2009</cite>]]></description></item><item><title>Lunar Dust Levitation</title><link>http://academic.research.microsoft.com/Publication/26912588</link><pubDate>Mon, 20 May 2013 14:31:11 GMT</pubDate><guid isPermaLink="false">26912588</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/55563423">Joshua E. Colwell</a>, <a href="http://academic.research.microsoft.com/Author/22237830">Scott R. Robertson</a>, <a href="http://academic.research.microsoft.com/Author/709211">Mihály Horányi</a>, <a href="http://academic.research.microsoft.com/Author/24461601">Xu Wang</a>, <a href="http://academic.research.microsoft.com/Author/21882654">Andrew Poppe</a>, <a href="http://academic.research.microsoft.com/Author/2512320">Patrick Wheeler</a><span style="margin-left:20px">(Citations:6)</span><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i1/p2/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 1, 2009</cite>]]></description></item><item><title>Explicit Finite-Element Analysis of 2024-T3/T351 Aluminum Material under Impact Loading for Airplane Engine Containment and Fragment Shielding</title><link>http://academic.research.microsoft.com/Publication/26912615</link><pubDate>Mon, 20 May 2013 14:31:10 GMT</pubDate><guid isPermaLink="false">26912615</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/22001092">Murat Buyuk</a>, <a href="http://academic.research.microsoft.com/Author/5819443">Steve Kan</a>, <a href="http://academic.research.microsoft.com/Author/23330847">Matti J. Loikkanen</a><span style="margin-left:20px">(Citations:2)</span><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i3/p287/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 3, 2009</cite>]]></description></item><item><title>Design of a Static Thruster for Microair Vehicle Rotorcraft</title><link>http://academic.research.microsoft.com/Publication/26912596</link><pubDate>Mon, 20 May 2013 14:31:09 GMT</pubDate><guid isPermaLink="false">26912596</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/4400608">Paul E. I. Pounds</a>, <a href="http://academic.research.microsoft.com/Author/1666385">Robert E. Mahony</a>, <a href="http://academic.research.microsoft.com/Author/906299">Peter I. Corke</a><span style="margin-left:20px">(Citations:1)</span><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i1/p85/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 1, 2009</cite>]]></description></item><item><title>Dynamic Loads in the Fan Containment Structure of a Turbofan Engine</title><link>http://academic.research.microsoft.com/Publication/26912612</link><pubDate>Mon, 20 May 2013 14:31:08 GMT</pubDate><guid isPermaLink="false">26912612</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/6866258">Sunil K. Sinha</a>, <a href="http://academic.research.microsoft.com/Author/22237855">Sreekanth Dorbala</a><span style="margin-left:20px">(Citations:2)</span><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i3/p260/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 3, 2009</cite>]]></description></item><item><title>Model for Granular Materials with Surface Energy Forces</title><link>http://academic.research.microsoft.com/Publication/26912591</link><pubDate>Mon, 20 May 2013 14:31:07 GMT</pubDate><guid isPermaLink="false">26912591</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/12664715">C. S. Chang</a>, <a href="http://academic.research.microsoft.com/Author/21838044">P.-Y. Hicher</a><span style="margin-left:20px">(Citations:1)</span><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i1/p43/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 1, 2009</cite>]]></description></item><item><title>A Unified Approach to the Characterization of Coupled Composite Laminates: Benchmark Configurations and Special Cases</title><link>http://academic.research.microsoft.com/Publication/26912638</link><pubDate>Mon, 20 May 2013 14:31:06 GMT</pubDate><guid isPermaLink="false">26912638</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/21837557">C. B. York</a><span style="margin-left:20px">(Citations:1)</span><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000036">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2009</cite>]]></description></item><item><title>New Approach to Satellite Formation-Keeping: Exact Solution to the Full Nonlinear Problem</title><link>http://academic.research.microsoft.com/Publication/26912633</link><pubDate>Mon, 20 May 2013 14:31:05 GMT</pubDate><guid isPermaLink="false">26912633</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/3984831">Hancheol Cho</a>, <a href="http://academic.research.microsoft.com/Author/22237868">Adam Yu</a><span style="margin-left:20px">(Citations:1)</span><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i4/p445/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 4, 2009</cite>]]></description></item><item><title>Robust Backstepping Sliding Mode Attitude Tracking and Vibration Damping of Flexible Spacecraft with Actuator Dynamics</title><link>http://academic.research.microsoft.com/Publication/26912602</link><pubDate>Mon, 20 May 2013 14:31:04 GMT</pubDate><guid isPermaLink="false">26912602</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/12961509">Qinglei Hu</a>, <a href="http://academic.research.microsoft.com/Author/53641625">Jun Cao</a>, <a href="http://academic.research.microsoft.com/Author/56474581">Yizhuo Zhang</a><span style="margin-left:20px">(Citations:1)</span><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i2/p139/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 2, 2009</cite>]]></description></item><item><title>Investigation of the Influence of Pseudoinverse Matrix Calculations on Multibody Dynamics Simulations by Means of the Udwadia-Kalaba Formulation</title><link>http://academic.research.microsoft.com/Publication/26912624</link><pubDate>Mon, 20 May 2013 14:31:03 GMT</pubDate><guid isPermaLink="false">26912624</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/56630293">D. de Falco</a>, <a href="http://academic.research.microsoft.com/Author/12929908">E. Pennestrì</a>, <a href="http://academic.research.microsoft.com/Author/12929910">L. Vita</a><span style="margin-left:20px">(Citations:1)</span><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i4/p365/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 4, 2009</cite>]]></description></item><item><title>NAO1: Lunar Highland Soil Simulant Developed in China</title><link>http://academic.research.microsoft.com/Publication/26912592</link><pubDate>Mon, 20 May 2013 14:31:02 GMT</pubDate><guid isPermaLink="false">26912592</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/53753264">Yongquan Li</a>, <a href="http://academic.research.microsoft.com/Author/53717274">Jianzhong Liu</a>, <a href="http://academic.research.microsoft.com/Author/22237837">Zongyu Yue</a><span style="margin-left:20px">(Citations:1)</span><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i1/p53/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 1, 2009</cite>]]></description></item><item><title>Membrane Micro Air Vehicles with Adaptive Aerodynamic Twist: Numerical Modeling</title><link>http://academic.research.microsoft.com/Publication/26912605</link><pubDate>Mon, 20 May 2013 14:31:01 GMT</pubDate><guid isPermaLink="false">26912605</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/13019011">Bret Stanford</a>, <a href="http://academic.research.microsoft.com/Author/11101586">Peter Ifju</a><span style="margin-left:20px">(Citations:1)</span><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i2/p173/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 2, 2009</cite>]]></description></item><item><title>Shuttle Debris Impact Analysis: Postreturn to Flight Real-Time Mission Support</title><link>http://academic.research.microsoft.com/Publication/26912609</link><pubDate>Mon, 20 May 2013 14:31:00 GMT</pubDate><guid isPermaLink="false">26912609</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/22237848">Jason L. Firko</a>, <a href="http://academic.research.microsoft.com/Author/5324818">Jeremie J. Albert</a>, <a href="http://academic.research.microsoft.com/Author/42958633">Timothy J. Lee</a>, <a href="http://academic.research.microsoft.com/Author/22237851">Alexander M. Boyer</a>, <a href="http://academic.research.microsoft.com/Author/34268904">Jonathan W. Gabrys</a>, <a href="http://academic.research.microsoft.com/Author/55323822">Kelly S. Carney</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i3/p222/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 3, 2009</cite>]]></description></item><item><title>Generalized, Three-Dimensional Definition, Description, and Derived Limits of the Triaxial Failure of Metals</title><link>http://academic.research.microsoft.com/Publication/26912614</link><pubDate>Mon, 20 May 2013 14:30:59 GMT</pubDate><guid isPermaLink="false">26912614</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/55323822">Kelly S. Carney</a>, <a href="http://academic.research.microsoft.com/Author/22237856">Paul A. DuBois</a>, <a href="http://academic.research.microsoft.com/Author/22001092">Murat Buyuk</a>, <a href="http://academic.research.microsoft.com/Author/5819443">Steve Kan</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i3/p280/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 3, 2009</cite>]]></description></item><item><title>Computational Methodology for Modeling Fracture in Fiber-Reinforced Polymer Composites</title><link>http://academic.research.microsoft.com/Publication/26912616</link><pubDate>Mon, 20 May 2013 14:30:58 GMT</pubDate><guid isPermaLink="false">26912616</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/53517815">A. A. Benzerga</a>, <a href="http://academic.research.microsoft.com/Author/22237859">X. Poulain</a>, <a href="http://academic.research.microsoft.com/Author/54179869">K. A. Chowdhury</a>, <a href="http://academic.research.microsoft.com/Author/21717159">R. Talreja</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i3/p296/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 3, 2009</cite>]]></description></item><item><title>Numerical Implementation of Polymer Viscoplastic Equations for High Strain-Rate Composite Models</title><link>http://academic.research.microsoft.com/Publication/26912617</link><pubDate>Mon, 20 May 2013 14:30:57 GMT</pubDate><guid isPermaLink="false">26912617</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/21814321">Pablo A. Salas</a>, <a href="http://academic.research.microsoft.com/Author/52561216">David J. Benson</a>, <a href="http://academic.research.microsoft.com/Author/12827893">Satchi Venkataraman</a>, <a href="http://academic.research.microsoft.com/Author/23330847">Matti J. Loikkanen</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i3/p304/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 3, 2009</cite>]]></description></item><item><title>Assignment of Geometrical and Physical Parameters for the Confinement of Vibrations in Flexible Structures</title><link>http://academic.research.microsoft.com/Publication/26912628</link><pubDate>Mon, 20 May 2013 14:30:56 GMT</pubDate><guid isPermaLink="false">26912628</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/22237865">W. Gafsi</a>, <a href="http://academic.research.microsoft.com/Author/22159812">S. Choura</a>, <a href="http://academic.research.microsoft.com/Author/12668960">A. Nayfeh</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i4/p403/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 4, 2009</cite>]]></description></item><item><title>Structural Design Considerations of an Inflatable Rigidizable Space Shuttle Experiment</title><link>http://academic.research.microsoft.com/Publication/26912600</link><pubDate>Mon, 20 May 2013 14:30:55 GMT</pubDate><guid isPermaLink="false">26912600</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/22237844">Raymond G. Holstein</a>, <a href="http://academic.research.microsoft.com/Author/7809175">Anthony N. Palazotto</a>, <a href="http://academic.research.microsoft.com/Author/22237804">Richard G. Cobb</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i2/p123/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 2, 2009</cite>]]></description></item><item><title>Feasibility Study of Rotorcraft Fire Fighting for High-Rise Buildings</title><link>http://academic.research.microsoft.com/Publication/5440230</link><pubDate>Mon, 20 May 2013 14:30:54 GMT</pubDate><guid isPermaLink="false">5440230</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/42117808">Erminio Zanenga</a>, <a href="http://academic.research.microsoft.com/Author/3139788">Domenico Leonello</a>, <a href="http://academic.research.microsoft.com/Author/12863913">Carlo L. Bottasso</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000021">view publication</a></span></p><p>Fire risk in high-rise buildings is of special concern to the fire community, since it is crucial but still technically extremely challenging to significantly improve the current fire fighting capabilities when a calamity happens above the "seven storey limit". In fact, at the moment there is a lack of effective means for fire fighting in this rare but potentially ...</p><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2009</cite>]]></description></item><item><title>Overview of the National Aeronautics and Space Administration Subsonic Rotary Wing Aeronautics Research Program in Rotorcraft Crashworthiness</title><link>http://academic.research.microsoft.com/Publication/26912610</link><pubDate>Mon, 20 May 2013 14:30:53 GMT</pubDate><guid isPermaLink="false">26912610</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/8772666">Karen E. Jackson</a>, <a href="http://academic.research.microsoft.com/Author/18427614">Yvonne T. Fuchs</a>, <a href="http://academic.research.microsoft.com/Author/18134967">Sotiris Kellas</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i3/p229/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 3, 2009</cite>]]></description></item><item><title>Orion Crew Member Injury Predictions during Land and Water Landings</title><link>http://academic.research.microsoft.com/Publication/12018019</link><pubDate>Mon, 20 May 2013 14:30:52 GMT</pubDate><guid isPermaLink="false">12018019</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/64358">Charles Lawrence</a>, <a href="http://academic.research.microsoft.com/Author/13360428">Justin D. Littell</a>, <a href="http://academic.research.microsoft.com/Author/12930310">Edwin L. Fasanella</a>, <a href="http://academic.research.microsoft.com/Author/12823681">Ala Tabiei</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://gltrs.grc.nasa.gov/reports/2008/TM-2008-215171.pdf">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 3, 2009</cite>]]></description></item><item><title>Continuum Modeling and Discrete Element Simulations of Elastic-Quasi-Static Granular Flow in a Compressing Slot</title><link>http://academic.research.microsoft.com/Publication/26912629</link><pubDate>Mon, 20 May 2013 14:30:51 GMT</pubDate><guid isPermaLink="false">26912629</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/10721015">B. T. Helenbrook</a>, <a href="http://academic.research.microsoft.com/Author/25064441">M. Powers</a>, <a href="http://academic.research.microsoft.com/Author/19398953">H. H. Shen</a>, <a href="http://academic.research.microsoft.com/Author/48249529">P. T. Metzger</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i4/p415/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 4, 2009</cite>]]></description></item><item><title>Oscillation Susceptibility Analysis along the Path of the Longitudinal Flight Equilibriums in ADMIRE Model</title><link>http://academic.research.microsoft.com/Publication/26912630</link><pubDate>Mon, 20 May 2013 14:30:50 GMT</pubDate><guid isPermaLink="false">26912630</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/13209600">Stefan Balint</a>, <a href="http://academic.research.microsoft.com/Author/13209601">Agneta M. Balint</a>, <a href="http://academic.research.microsoft.com/Author/22613412">Achim Ioniţă</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i4/p423/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 4, 2009</cite>]]></description></item><item><title>Finite-Element Analysis of Lamb Wave Propagation in a Thin Aluminum Plate</title><link>http://academic.research.microsoft.com/Publication/26912606</link><pubDate>Mon, 20 May 2013 14:30:49 GMT</pubDate><guid isPermaLink="false">26912606</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/53513732">SeJin Han</a>, <a href="http://academic.research.microsoft.com/Author/7809175">Anthony N. Palazotto</a>, <a href="http://academic.research.microsoft.com/Author/22268604">Charles L. Leakeas</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i2/p185/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 2, 2009</cite>]]></description></item><item><title>Simplified Impedance Model for Adhesively Bonded Piezo-Impedance Transducers</title><link>http://academic.research.microsoft.com/Publication/26912625</link><pubDate>Mon, 20 May 2013 14:30:48 GMT</pubDate><guid isPermaLink="false">26912625</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/13200463">Suresh Bhalla</a>, <a href="http://academic.research.microsoft.com/Author/12471952">Praveen Kumar</a>, <a href="http://academic.research.microsoft.com/Author/10587447">Ashok Gupta</a>, <a href="http://academic.research.microsoft.com/Author/54211017">Tushar K. Datta</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i4/p373/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 4, 2009</cite>]]></description></item><item><title>Finite-Element Analysis of the Influence of Edge Geometry on Shot Peening Process</title><link>http://academic.research.microsoft.com/Publication/26912603</link><pubDate>Mon, 20 May 2013 14:30:47 GMT</pubDate><guid isPermaLink="false">26912603</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/12555935">Jifeng Xu</a>, <a href="http://academic.research.microsoft.com/Author/22237846">William J. Koch</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i2/p153/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 2, 2009</cite>]]></description></item><item><title>Case Study: Planar Kinematics of Dragline for Efficient Machine Control</title><link>http://academic.research.microsoft.com/Publication/26912599</link><pubDate>Mon, 20 May 2013 14:30:46 GMT</pubDate><guid isPermaLink="false">26912599</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/21723359">Samuel Frimpong</a>, <a href="http://academic.research.microsoft.com/Author/50987838">Nuray Demirel</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i2/p112/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 2, 2009</cite>]]></description></item><item><title>Characterization of Damage in Triaxial Braided Composites under Tensile Loading</title><link>http://academic.research.microsoft.com/Publication/26912613</link><pubDate>Mon, 20 May 2013 14:30:45 GMT</pubDate><guid isPermaLink="false">26912613</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/13360428">Justin D. Littell</a>, <a href="http://academic.research.microsoft.com/Author/7873767">Wieslaw K. Binienda</a>, <a href="http://academic.research.microsoft.com/Author/18474049">Gary D. Roberts</a>, <a href="http://academic.research.microsoft.com/Author/18474048">Robert K. Goldberg</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i3/p270/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 3, 2009</cite>]]></description></item><item><title>Real-Time Optimized Trajectory Planning for a Fixed-Wing Vehicle Flying in a Dynamic Environment</title><link>http://academic.research.microsoft.com/Publication/26912621</link><pubDate>Mon, 20 May 2013 14:30:44 GMT</pubDate><guid isPermaLink="false">26912621</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/47341373">Jian Yang</a>, <a href="http://academic.research.microsoft.com/Author/18186775">Zhihua Qu</a>, <a href="http://academic.research.microsoft.com/Author/2371748">Jing Wang</a>, <a href="http://academic.research.microsoft.com/Author/13017510">Richard A. Hull</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i4/p331/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 4, 2009</cite>]]></description></item><item><title>Response of an Elastic Structure Subject to Air Shock Considering Fluid-Structure Interaction</title><link>http://academic.research.microsoft.com/Publication/26912637</link><pubDate>Mon, 20 May 2013 14:30:43 GMT</pubDate><guid isPermaLink="false">26912637</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/22001237">Weimin Nian</a>, <a href="http://academic.research.microsoft.com/Author/18378777">Kolluru Subramaniam</a>, <a href="http://academic.research.microsoft.com/Author/337342">Yiannis Andreopoulos</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000022">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2009</cite>]]></description></item><item><title>Methodology for Impact Modeling of Triaxial Braided Composites Using Shell Elements</title><link>http://academic.research.microsoft.com/Publication/26912618</link><pubDate>Mon, 20 May 2013 14:30:42 GMT</pubDate><guid isPermaLink="false">26912618</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/43228303">Xuetao Li</a>, <a href="http://academic.research.microsoft.com/Author/7873767">Wieslaw K. Binienda</a>, <a href="http://academic.research.microsoft.com/Author/13360428">Justin D. Littell</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i3/p310/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 3, 2009</cite>]]></description></item><item><title>Autopilot for Reconfigurable Flight Control System</title><link>http://academic.research.microsoft.com/Publication/26912595</link><pubDate>Mon, 20 May 2013 14:30:41 GMT</pubDate><guid isPermaLink="false">26912595</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/22237838">M. Zugaj</a>, <a href="http://academic.research.microsoft.com/Author/10498668">J. Narkiewicz</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i1/p78/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 1, 2009</cite>]]></description></item><item><title>Nondetection, False Alarm, and Calibration Insensitivity in Kurtosis and Pseudofractal-Based Singularity Detection</title><link>http://academic.research.microsoft.com/Publication/26912636</link><pubDate>Mon, 20 May 2013 14:30:40 GMT</pubDate><guid isPermaLink="false">26912636</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/21677419">Vikram Pakrashi</a>, <a href="http://academic.research.microsoft.com/Author/12855875">Biswajit Basu</a>, <a href="http://academic.research.microsoft.com/Author/34264333">Alan O’Connor</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i4/p466/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 4, 2009</cite>]]></description></item><item><title>Asymptotic Approach to Free Beam Vibration Analysis</title><link>http://academic.research.microsoft.com/Publication/26912634</link><pubDate>Mon, 20 May 2013 14:30:39 GMT</pubDate><guid isPermaLink="false">26912634</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/21806095">G. V. Kostin</a>, <a href="http://academic.research.microsoft.com/Author/21806096">V. V. Saurin</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i4/p456/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 4, 2009</cite>]]></description></item><item><title>Computer Modeling for the Complex Response Analysis of Nonstandard Structural Dynamics Problems</title><link>http://academic.research.microsoft.com/Publication/26912620</link><pubDate>Mon, 20 May 2013 14:30:38 GMT</pubDate><guid isPermaLink="false">26912620</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/22237862">Abhimanyu Kumar</a>, <a href="http://academic.research.microsoft.com/Author/13051128">Atef F. Saleeb</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i3/p324/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 3, 2009</cite>]]></description></item><item><title>Comprehensive Modeling of Shape Memory Alloy Material Response Using a Multimechanism-Based Inelastic Model</title><link>http://academic.research.microsoft.com/Publication/26912632</link><pubDate>Mon, 20 May 2013 14:30:37 GMT</pubDate><guid isPermaLink="false">26912632</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/13051128">Atef F. Saleeb</a>, <a href="http://academic.research.microsoft.com/Author/22237862">Abhimanyu Kumar</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i4/p438/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 4, 2009</cite>]]></description></item><item><title>Semianalytical Solution of Wave-Controlled Impact on Composite Laminates</title><link>http://academic.research.microsoft.com/Publication/26912619</link><pubDate>Mon, 20 May 2013 14:30:36 GMT</pubDate><guid isPermaLink="false">26912619</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/52906112">D. Zheng</a>, <a href="http://academic.research.microsoft.com/Author/7873767">W. K. Binienda</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i3/p318/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 3, 2009</cite>]]></description></item><item><title>Two-Dimensional Simulation of the Angle of Repose for a Particle System with Electrostatic Charge under Lunar and Earth Gravity</title><link>http://academic.research.microsoft.com/Publication/26912587</link><pubDate>Mon, 20 May 2013 14:30:35 GMT</pubDate><guid isPermaLink="false">26912587</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/22216913">Shunying Ji</a>, <a href="http://academic.research.microsoft.com/Author/19398953">Hayley H. Shen</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i1/p10/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 1, 2009</cite>]]></description></item><item><title>Rendezvous Guidance Trajectories via Multiple-Subarc Sequential Gradient-Restoration Algorithm</title><link>http://academic.research.microsoft.com/Publication/26912604</link><pubDate>Mon, 20 May 2013 14:30:34 GMT</pubDate><guid isPermaLink="false">26912604</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/21645764">A. Miele</a>, <a href="http://academic.research.microsoft.com/Author/22157916">M. Ciarcià</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/JAEEEZ/v22/i2/p160/s1&Agg=doi">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, vol. 22, no. 2, 2009</cite>]]></description></item><item><title>The Flutter of a Swept Aircraft Wing with a Powered-Engine</title><link>http://academic.research.microsoft.com/Publication/26912640</link><pubDate>Mon, 20 May 2013 14:30:33 GMT</pubDate><guid isPermaLink="false">26912640</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/21727713">A. Mazidi</a>, <a href="http://academic.research.microsoft.com/Author/21842861">S. A. Fazelzadeh</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000037">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2009</cite>]]></description></item><item><title>Inverse First-Order Reliability Method for Probabilistic Fatigue Life Prediction of Composite Laminates under Multiaxial Loading</title><link>http://academic.research.microsoft.com/Publication/26912641</link><pubDate>Mon, 20 May 2013 14:30:32 GMT</pubDate><guid isPermaLink="false">26912641</guid><description><![CDATA[<p><a href="http://academic.research.microsoft.com/Author/42573294">Yibing Xiang</a>, <a href="http://academic.research.microsoft.com/Author/12983182">Yongming Liu</a><span style="margin-left:20px" /><span style="margin-left:20px"><a href="http://link.aip.org/link/doi/10.1061/(ASCE)AS.1943-5525.0000023">view publication</a></span></p><p /><cite></cite><cite>Journal: <a href="http://academic.research.microsoft.com/Journal/5477">Journal of Aerospace Engineering - J AEROSP ENG</a>, 2009</cite>]]></description></item></channel></rss>