AIAA 90-1946 - AIAA 90-1985
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Total Pages | : 338 |
Release | : 1990 |
Genre | : Airplanes |
ISBN | : |
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Author | : |
Publisher | : |
Total Pages | : 338 |
Release | : 1990 |
Genre | : Airplanes |
ISBN | : |
Author | : |
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Total Pages | : 530 |
Release | : 1990 |
Genre | : Heat |
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Author | : Thomas J. Mueller |
Publisher | : AIAA |
Total Pages | : 614 |
Release | : 2001 |
Genre | : Aerodynamics |
ISBN | : 9781600864469 |
This title reports on the latest research in the area of aerodynamic efficency of various fixed-wing, flapping wing, and rotary wing concepts. It presents the progress made by over fifty active researchers in the field.
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Total Pages | : |
Release | : 1990 |
Genre | : Airplanes |
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Total Pages | : 514 |
Release | : 1990 |
Genre | : Fluid dynamics |
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Author | : Holger Babinsky |
Publisher | : Cambridge University Press |
Total Pages | : 481 |
Release | : 2011-09-12 |
Genre | : Technology & Engineering |
ISBN | : 1139498649 |
Shock wave-boundary-layer interaction (SBLI) is a fundamental phenomenon in gas dynamics that is observed in many practical situations, ranging from transonic aircraft wings to hypersonic vehicles and engines. SBLIs have the potential to pose serious problems in a flowfield; hence they often prove to be a critical - or even design limiting - issue for many aerospace applications. This is the first book devoted solely to a comprehensive, state-of-the-art explanation of this phenomenon. It includes a description of the basic fluid mechanics of SBLIs plus contributions from leading international experts who share their insight into their physics and the impact they have in practical flow situations. This book is for practitioners and graduate students in aerodynamics who wish to familiarize themselves with all aspects of SBLI flows. It is a valuable resource for specialists because it compiles experimental, computational and theoretical knowledge in one place.
Author | : American Institute of Aeronautics and Astronautics. Technical Information Service |
Publisher | : |
Total Pages | : 180 |
Release | : 1990 |
Genre | : AIAA paper |
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Total Pages | : |
Release | : 1985 |
Genre | : Aeronautics |
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Total Pages | : |
Release | : 1985 |
Genre | : Aeronautics |
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Total Pages | : 24 |
Release | : 2002 |
Genre | : Air-supported structures |
ISBN | : |
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.