Sign in
Author
|
Conference
|
Journal
|
Organization
|
Year
|
DOI
Look for results that meet for the following criteria:
since
equal to
before
between
and
Search in all fields of study
Limit my searches in the following fields of study
Agriculture Science
Arts & Humanities
Biology
Chemistry
Computer Science
Economics & Business
Engineering
Environmental Sciences
Geosciences
Material Science
Mathematics
Medicine
Physics
Social Science
Multidisciplinary
Subscribe
Academic
Publications
Introduction to Flight
Introduction to Flight,10.1063/1.2820235,Physics Today,John D. Anderson,Lloyd P. Hunter
Edit
Introduction to Flight
(
Citations: 79
)
BibTex
|
RIS
|
RefWorks
Download
John D. Anderson
,
Lloyd P. Hunter
Journal:
Physics Today - PHYS TODAY
, vol. 40, no. 10, 1987
DOI:
10.1063/1.2820235
Cumulative
Annual
View Publication
The following links allow you to view full publications. These links are maintained by other sources not affiliated with Microsoft Academic Search.
(
link.aip.org
)
Citation Context
(25)
...;
Anderson, 2000
...
Gilles Labonté
.
Formulas for the fuel of climbing propeller driven airplanes
...It is stated in [
21
] that an isentropic process is one in which there is neither heat exchange nor any effect due to friction...
...Under the assumption that the viscosity of the flow around a subsonic airplane is negligible, the dynamic characteristic of the wake can be characterized by the Euler equation [
21
, 22]...
Jianbing Li
,
et al.
Modeling the Dielectric Constant Distribution of Wake Vortices
...where hattack is the angle of attack of the rudder [2, 3,
24
, 25]...
Ray-Qing Lin
,
et al.
Prediction of ship steering capabilities with a fully nonlinear ship m...
...The concept of static stability of airplanes [11], [12], [13], [
14
] is helpful in defining this step...
...The concept of dynamic stability of airplanes [11], [12], [13], [
14
] is helpful in defining this step...
Rush D. Robinett
,
et al.
Transient stability and control of renewable generators based on Hamil...
...These equations are well known[
1
] and are not the purpose of this paper...
...The frequency spectrum analysis (Figure 5) shows that, based on the well known Nyquist-Shannon[
1
] sampling theorem, in this flight only 2 Hz are required...
...In Figure 6, the frequency spectrum shows the existence of an oscillator in the band corresponding to a Phugoid mode[
1
]...
Joshua Tristancho
,
et al.
A telemetry modeling for intelligent UAV monitoring
Sort by:
Citations
(79)
Formulas for the fuel of climbing propeller driven airplanes
Gilles Labonté
Journal:
Aircraft Engineering and Aerospace Technology - AIRCRAFT ENG AEROSP TECHNOL
, vol. 84, no. 1, pp. 23-36, 2012
New insights into amblyopia: Perceptual deficits and treatment
Agnes Wong
,
Robert Hess
,
Benjamin Thompson
Journal:
Journal of Aapos - J AAPOS
, vol. 15, no. 1, pp. e39-e40, 2011
Modeling the Dielectric Constant Distribution of Wake Vortices
Jianbing Li
,
Xuesong Wang
,
Tao Wang
Journal:
IEEE Transactions on Aerospace and Electronic Systems - IEEE TRANS AEROSP ELECTRON SY
, vol. 47, no. 2, pp. 820-831, 2011
Project-based introduction to aerospace engineering course: A model rocket
Sanjay Jayaram
,
Lawrence Boyer
,
John George
,
K. Ravindra
,
Kyle Mitchell
Journal:
Acta Astronautica - ACTA ASTRONAUT
, vol. 66, no. 9, pp. 1525-1533, 2010
Prediction of ship steering capabilities with a fully nonlinear ship motion model. Part 1: Maneuvering in calm water
Ray-Qing Lin
,
Michael Hughes
,
Tim Smith
Journal:
Journal of Marine Science and Technology - J MAR SCI TECHNOL
, vol. 15, no. 2, pp. 131-142, 2010