The development of analytical and experimental techniques needed to predict space shuttle flutter boundaries and insure adequate flutter margins and anticipated problems associated with aeroelastic-model and full-scale testing to validate flutter clearance are considered. Results illustrating the best available tools for subsonic and supersonic flutter prediction are presented. Programs currently underway which will help overcome the difficult problems envisioned for the transonic wind-tunnel and flight flutter test program are also discussed.


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    Title :

    Flutter technology for space shuttle


    Contributors:


    Publication date :

    1972-07-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :



    Space Shuttle Flutter as Affected by Wing-Body Aerodynamic Interaction

    R. R. Chipman / F. J. Rauch / P. Shyprykevich et al. | AIAA | 1975


    Space Shuttle flutter as affected by wing-body aerodynamic interaction

    CHIPMAN, R. / RAUCH, F. / SHYPRYKEVICH, P. et al. | AIAA | 1974


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    Chipman, R. R. / Rauch, F. J. / Shyprykevich, P. et al. | NTRS | 1974