This report presents the results of a state-of-the-art study on pressure and heat-transfer distribuions on axisymmetric bodies in the high Reynolds number per foot regime. The Mach number range covered is generally from 3.5 to 9 corresponding to the flight envelope of the Army Missile Command low-altitude/high-velocity experiment (LAHIVE). In addition to a summary of previous flight and wind-tunnel data, areas of controversy and unexplained or anomalous results are pointed out in which LAHIVE data will be of great value. A brief survey is presented of Government-owned wind tunnels, ranges, and shock tunnels pertinent to the LAHIVE flight regime. Recommendations on instrumentations are included, particularly for the cone-cylinder-flare vehicles, on the data analysis and correlation of results, and on further applications of LAHIVE vehicles. (Author)


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    Titel :

    A Critical Review of Data on Heat Transfer and Pressure Distribution on Nose Cones in the High Unit Reynolds Number Regime


    Beteiligte:
    G. R. Whitacre (Autor:in) / E. W. Ungar (Autor:in)

    Erscheinungsdatum :

    1967


    Format / Umfang :

    71 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch