Author: Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 310
Book Description
AIAA Aircraft Design Systems Meeting: 92-4221 - 92-4250
Author: AIAA Aircraft Design Systems Meeting: 92-4188 - 92-4220
Author: AIAA Aircraft Design Systems and Operations Meeting: 93-3970 - 93-4023 (93-4735)
Author: AIAA Aircraft Design Systems Meeting: 92-4251
Author: AIAA Aircraft Design Systems and Operations Meeting: 93-3916 - 93-3968
Author: AIAA Aircraft Design Systems and Operations Meeting: 91-3133 - 91-3194
Author: AIAA Aircraft Design Systems and Operations Meeting: 91-3074 - 91-3130
Author: AIAA Aerospace Design Engineers Guide
Author: AIAA (American Institute of Aeronautics and Astronautics)Publisher: John Wiley & Sons
ISBN: 9781860584244
Category : Technology & Engineering
Languages : en
Pages : 456
Book Description
An indispensable reference for aerospace designers, analysts and students. This fifth revised and enlarged edition of this classic, indispensable, and practical guide provides a condensed collection of commonly used engineering reference data specifically related to aerospace design. New material on air breathing propulsion, systems engineering, and radar cross section has been added to reflect recent data in aircraft design. Features: New material on air breathing propulsion, systems engineering, and radar cross section Most commonly used formulas and data for aerospace design Convenient size and binding Large, easy-to-read tables, charts, and figures Handy reference for everyday use Developed by aerospace professionals AIAA Aerospace Design Engineers Guide is an essential tool for every design engineer and every aspiring aerospace engineering student.
AIAA Aircraft Design Systems and Operations Meeting
Author: 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.