Author: Publisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 672
Book Description
AIAA 76-487 - AIAA 76-530
Author: Aeronautical Engineering
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 916
Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
AIAA 76-92 - AIAA 76-207. (With omissions in numbering)
Author: AIAA 76-1 - AIAA 76-91
Author: AIAA 76-674 - AIAA 76-774. (With omissions in numbering)
Author: AIAA 76-595 - AIAA 76-673
Author: AIAA 78-1 - AIAA 78-76
Author: International Aerospace Abstracts
Author: Elements of Aviation Acoustics
Author: G. J. J. RuijgrokPublisher: IOS Press
ISBN:
Category : Science
Languages : en
Pages : 360
Book Description
"The purpose of this book is to provide insight into those elements of acoustics and aeronautics that are connected directly with the problem of aviation noise. It is intended as a textbook for a university course on aviation acoustics at an undergraduate level. The simplicity of presentation also lends itself to the book's use as an instrument of selfstudy for the practicing engineer. The contents of the book are a reflection of an annual course on aviation noise presented by the author to senior undergraduate students of aerospace engineering at Delft University of Technology."--BOOK JACKET.
Ground and Flight Evaluation of a Small-Scale Inflatable-Winged Aircraft
Author: Publisher:
ISBN:
Category : Air-supported structures
Languages : en
Pages : 24
Book Description
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.