Comparison between experimental pressure distributions on inclined model airship hull and those calculated by nonviscous theory; problem is of more interest at present to missile and supersonic aircraft designers.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Pressure distribution and some effects of viscosity on slender inclined bodies of revolution


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Allen, H.J. (author)


    Publication date :

    1950


    Size :

    19 pages


    Remarks:

    Diagrs, Charts


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :