AIAA Aerospace Engineering Conference & Show
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Page : 114 pages
File Size : 14,84 MB
Release : 1990
Category : Aeronautics
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Author :
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Page : 114 pages
File Size : 14,84 MB
Release : 1990
Category : Aeronautics
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Page : pages
File Size : 41,60 MB
Release : 1990
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Page : pages
File Size : 13,54 MB
Release : 1987
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Author : American Institute of Aeronautics and Astronautics (New York, N.Y.)
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Page : pages
File Size : 16,49 MB
Release : 1984
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Page : pages
File Size : 39,53 MB
Release : 1985
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Author : American Institute of Aeronautics and Astronautics
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
Page : 526 pages
File Size : 46,49 MB
Release : 1997
Category : Technology & Engineering
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Topics for the 1997 conference on modelling and simulation technologies included: motion systems; rotor-craft and air cushion vehicle dynamics and modelling; pilot training and low-cost simulation; weapons and engagement modelling and simulation; simulator network and information technologies; visual, radarf and environmental modelling and simulation; test and evaluation; space systems; simulator fidelity; aircraft dynamics, modelling and performance; simulator development and software re-use; human factors; and research and test facilities.
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Page : 480 pages
File Size : 26,57 MB
Release : 1992
Category : Airplanes
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Page : 24 pages
File Size : 19,46 MB
Release : 2002
Category : Air-supported structures
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A small-scale, instrumented research aircraft was flown to investigate the flight characteristics of inflatable wings. Ground tests measured the static structural characteristics of the wing at different inflation pressures, and these results compared favorably with analytical predictions. A research-quality instrumentation system was assembled, largely from commercial off-the-shelf components, and installed in the aircraft. Initial flight operations were conducted with a conventional rigid wing having the same dimensions as the inflatable wing. Subsequent flights were conducted with the inflatable wing. Research maneuvers were executed to identify the trim, aerodynamic performance, and longitudinal stability and control characteristics of the vehicle in its different wing configurations. For the angle-of-attack range spanned in this flight program.
Author : Thomas R. Yechout
Publisher : AIAA
Page : 666 pages
File Size : 33,78 MB
Release : 2003
Category : Aerodynamics
ISBN : 9781600860782
Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.
Author : E. T. Curran
Publisher : AIAA
Page : 1354 pages
File Size : 17,86 MB
Release : 2001
Category : Airplanes
ISBN : 9781600864414