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.


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    Title :

    Aeroelastic instability caused by slender payloads


    Additional title:

    J Spacecraft Rockets


    Contributors:

    Published in:

    Publication date :

    1967


    Size :

    9 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :