Theory presented in order to permit design of compressor blades which have high critical compression speeds. (15¢)


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    Title :

    Theory of unstaggered airfoil cascades in compressible flow


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:
    Spurr, R.A. (author) / Allen, H.J. (author)


    Publication date :

    1947


    Size :

    14 pages


    Remarks:

    Charts, Tables


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :