This report presents results of an investigation carried out in the Naval Ordnance Laboratory's Supersonic Tunnel Number 1 to determine the aerodynamic characteristics of the AGARD Calibration Model B. Tests were conducted at free-stream Mach numbers ranging from 0.70 to 3.50, at angles of attack from -4 to +10 degrees, over a Reynolds number range from 0.20 times 100to the 6th power to 0.62 times 10 to the 6th power. (Author)


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    Title :

    Wind Tunnel Measurements of the AGARD Calibration Model B at Transonic and Supersonic Speeds


    Contributors:
    J. B. Eades (author)

    Publication date :

    1964


    Size :

    24 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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