Study carried out at NAE to determine aerodynamic reactions on oscillating wings in hypersonic flows such as encountered in hypersonic gliders or re-entry vehicles; inviscid data were calculated for 2-dimensional wings and experiments undertaken to verify theoretical analysis and to determine effects of viscous flow phenomena; details of helium hypersonic wind tunnel constructed, calibration data and method of free oscillation used; experimental apparatus, model support and instrumentation.


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    Title :

    Oscillatory experiments in helium hypersonic wind tunnel


    Additional title:

    Canada. Nat Research Council -- Aeronautical Report


    Contributors:


    Publication date :

    1962


    Size :

    20 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :