Empirical anaytic methods are presented for calculating thermal and pressure distributions in three-dimensional, shock-wave turbulent-boundary-layer, interaction-flow regions on the surface of controllable hypersonic aircraft and missiles. The methods, based on several experimental investigations, are useful and reliable for estimating both the extent and magnitude of the increased thermal and pressure loads on the vehicle surfaces.


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    Titel :

    Methods for Estimating Pressure and Thermal Loads Induced by Elevon Deflections on Hypersonic-Vehicle Surfaces with Turbulent Boundary Layers


    Beteiligte:
    L. G. Kaufman (Autor:in) / C. B. Johnson (Autor:in)

    Erscheinungsdatum :

    1981


    Format / Umfang :

    41 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch