Report on flight tests to determine scale and compressibility effects on pressure distributions over wing having NA CA low drag profile; for lift coefficients ranging from 0 to 0.60, no appreciable compressibility effects on spanwise wing loading were noted below 0.75 Mach number; above this Mach number inboard lateral shift of load occurred.


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    Title :

    Wing pressure-distribution measurements up to 0,866 Mach number in flight on jet-propelled airplane


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1947


    Size :

    17 pages


    Remarks:

    Supp Plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :