Effects of Compressibility on Normal-Force, Pressure, and Load Characteristics of Tapered Wing of NACA 66-Series Airfoil Sections with Split Flaps.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Effects of compressibility on normal-force, pressure, and load characteristics of tapered wing of NACA 66-series airfoil sections with split flaps


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1948


    Size :

    44 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :