Analysis of mechanism for self-excited oscillations in boosters, covering linear and nonlinear amplitude effects produced by separation and reattachment of flow, as function of angle of attack; aerodynamic-coupling and control system effects are examined for several degrees of freedom.
Aeroelastic considerations in slender, blunt-nose, multistage rocket
Aerospace Eng
Aerospace Engineering ; 21 , n 5
1962
10 pages
Article (Journal)
English
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Aeroelastic analyses of multistage rocket systems
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