Analysis of unsteady aerodynamics associated with terminal shock occurring on cone-cylinder bodies at high subsonic speeds; quasi-steady techniques are used to account for effects of oscillations in bending or pitch on pressure gradient and boundary-layer buildup, i.e., on two parameters that control occurring flow separation; slender payload may, at high subsonic speeds, have aero-elastically destabilizing effects of two kinds; one is commonly occurring, linear, moderately undamping effect; other is rarely occurring, nonlinear, immensely undamping effect.
Aeroelastic instability caused by slender payloads
J Spacecraft Rockets
Journal of Spacecraft and Rockets ; 4 , n 1 ; p 65-73
1967
9 pages
Aufsatz (Zeitschrift)
Englisch
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Aeroelastic instability caused by slender payloads.
| AIAA | 1967
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| NTRS | 1967
Aeroelastic instability caused by slender payloads
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