Surface pressures were measured on plates with various values of angle of attack and of leading-edge sweep for Mach numbers of 4 and 5.7 and correlated for wide range of variables by method developed from boundary layer and blast-wave theory; method to predict variation in local Reynolds number with leading-edge sweep; applicability to trajectory of hypersonic winged vehicle in upper reaches of atmosphere.


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    Title :

    Effect of leading-edge sweep and surface inclination on hypersonic flow field over blunt flat plate


    Additional title:

    NASA -- Memo


    Contributors:


    Publication date :

    1959


    Size :

    45 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :