Theory of static aeroelastic stability of supersonic wings including chordwise bending, as previously developed, is further extended to include influence of stresses arising from thermal gradients.
Influence of thermal stresses on aeroelastic stability of supersonic wings
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 24 , n 6
1957
Aufsatz (Zeitschrift)
Englisch
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