Configurations considered are -- variable sweep wing; fixed wing, tail aft, 4 nacelles mounted on wing; fixed wing, canard Delta, trailing edge swept back 10°, leading edge swept back 60°, titanium wing and fuselage; fixed wing, canard Delta, trailing edge 0 °, leading edge 65°, steel wing and titanium fuselage; aerothermoelastic effects of sweep angle, wing thickness, "lg" working stress, and materials are shown; general considerations, such as probability predictions of survival of major structural component, fatigue spectrum considerations and estimations of magnitude of creep from 30,000 hr SST spectrum.
Design considerations for supersonic transport
SAE -- Paper
SAE Meeting ; 1963 Supersonic
1963
7 pages
Conference paper
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Design Considerations for a Supersonic Transport
SAE Technical Papers | 1964
|SUPERSONIC TRANSPORT DEVELOPMENT CONSIDERATIONS
SAE Technical Papers | 1975
|Design considerations for supersonic transport electric power system
Engineering Index Backfile | 1963
|Noise considerations in design and operation of supersonic transport
Engineering Index Backfile | 1961
|Commercial supersonic transport -- Some operational considerations
Engineering Index Backfile | 1961
|