Research undertaken at Langley 8-ft high speed tunnel to establish effects of variations of nose inlet proportions on critical Mach number. (35¢)


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    Title :

    Development and application of high-critical-speed nose inlets


    Additional title:

    Nat Advisory Committee Aeronautics -- Reports


    Contributors:
    Baals, D.D. (author) / Smith, N.F. (author) / Wright, J.B. (author)


    Publication date :

    1950


    Size :

    58 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



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