Presentation of all currently available force test data for airfoils obtained under same test conditions in Langley 24-in. high speed tunnel; airfoils tested over Mach number range from 0.3 to 0.8.


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    Title :

    Aerodynamic characteristics of 24 NACA 16-series airfoils at Mach numbers between 0.3 and 0.8


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1948


    Size :

    86 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :