Problems produced by aerodynamic heating and design approaches to help alleviate undesirable effects; loss of strength and creep at uniform elevated temperatures and effect of creep on airplane; non-uniform temperature distributions produced by changing flight conditions; buckling and loss of stiffness at stress levels well below those that produce buckling; design approaches to prevent stresses, and their adverse effects.
Some elevated temperature structural problems of high-speed aircraft
Soc Automotive Engrs -- Trans
1956
10 pages
Aufsatz (Zeitschrift)
Englisch
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