Analytical derivation of inlet shapes for maximum critical speed for given inlet velocity ratios; examples of resulting inlet shapes and of application to side or under wing scoops; shapes also suitable for axially symmetrical nose inlets. English translation from (ZWB) Forschungsbericht n 1209 Apr 15 1940.


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    Title :

    Two-dimensional symmetrical inlets with external compression


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Memo


    Contributors:
    Ruden, P. (author)


    Publication date :

    1950


    Size :

    48 pages


    Remarks:

    Diagrams, Charts


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :