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.


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    Title :

    Aeroelastic considerations in slender, blunt-nose, multistage rocket


    Additional title:

    Aerospace Eng


    Contributors:
    Woods, P. (author) / Ericsson, L. (author)

    Published in:

    Publication date :

    1962


    Size :

    10 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Aeroelastic analyses of multistage rocket systems

    Keith, J.S. / Lincoln, J.W. / Tarnower, G. | Engineering Index Backfile | 1961


    Aeroelastic Analyses of Multistage Rocket Systems

    J. S. Keith / J. W. Lincoln / G. Tarnower | NTIS | 1961



    Some static aeroelastic considerations of slender aircraft

    Hancock, G.J. | Engineering Index Backfile | 1961