Errors of 7 static-pressure probes mounted very close to nose of body of revolution were determined at Mach numbers from 0.80 to 1.08 and at angles of attack from -1.7° to 8.4°; 3 of probes were equipped with gimbal system and 4 vanes that aligned probe with local flow.


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    Title :

    Wind-tunnel tests of seven static-pressure probes at transonic speeds


    Additional title:

    NASA -- Tech Notes



    Publication date :

    1961


    Size :

    30 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :