Modes of failure found to be significant are considered which can be either aerodynamic, dynamic, structural, or combination of all 3; example of aero-thermal-elastic effects changing stability derivatives; when wing is exposed to loads and temperatures of selected flight profile, thermal deflections can be calculated using given temperature distribution; throughout mission profile, stability derivatives are changing and, thus, stability boundaries.
Modes of failure of hypersonic re-entry glide vehicle
Aerospace Eng
Aerospace Engineering ; 20 , n 9
1961
4 pages
Aufsatz (Zeitschrift)
Englisch
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