An experimental program was conducted in the AEDC-VKF hypervelocity Wind Tunnel (F) at a nominal Mach number of 19 to determine the static stability and axial-force characteristics of a 0.01-scale model of the NASA Space Shuttle Orbiter. The tests were conducted at an angle of attack of 30 deg at free-stream Reynolds numbers (based on model length) from 100000 to 400000. The results are compared to previous AEDC data at Mach numbers 8, 10, and 16. (Author)


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    Title :

    Viscous Effects on the Static Stability and Axial-Force Characteristics of the NASA Space Shuttle Orbiter at Mach Number 19


    Contributors:
    L. G. Siler (author)

    Publication date :

    1975


    Size :

    35 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English