A model is presented which enables one to determine the shape, the size, and the velocity of normal impact of a liquid droplet at the stagnation point of a blunt axisymmetric body in supersonic flight. (Author)


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    Title :

    Aerodynamic Aspects of Rain Erosion


    Contributors:
    E. Adams (author) / W. Koerner (author)

    Publication date :

    1971


    Size :

    17 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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