Paper shows that most efficient use of weight in vehicle design will only be achieved through examination of aerothermoelastic problem areas early in design cycle; emphasis is on effects associated with longitudinal stability and control of possible supersonic transport canard-delta configuration; flexible-to-rigid-ratio data obtained from modal techniques are presented for most major aerodynamic parameters at two loading conditions; direct influence coefficient approach provided additional insight into component mass and aerodynamic influences.
Aerothermoelasticity -- Its impact on stability and control of winged aerospace vehicles
J Aircraft
Journal of Aircraft ; 2 , n 6
1965
10 pages
Article (Journal)
English
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Static Aerothermoelasticity of Hypersonic Vehicles
AIAA | 2017
|Survey of aerothermoelasticity
Engineering Index Backfile | 1963
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