Results of experiments on unswept slab wing at nominal freestream Mach numbers of 7 and 10 show effect of distortions on heating and surface pressure at angles of attack up to 20°; wing, with both blunt and sharp leading edges, gives results over wide range of local Reynolds and Mach numbers; important alterations to heat-transfer distribution were obtained.


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    Title :

    Effect of surface distortions on heat transfer to wing at hypersonic speeds


    Additional title:

    AIAA J


    Contributors:
    Bertram, M.H. (author) / Wiggs, M.M. (author)

    Published in:

    AIAA Journal ; 1 , n 6


    Publication date :

    1963


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




    Hypersonic Heat Transfer on the Upper Wing Surface Fins

    Borovoy, V. / Kubyshina, R. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 1993


    Hypersonic heat transfer on the upper wing surface fins

    Borovoj, V. / Kubyshina, T. | AIAA | 1993