Wing ceases to deflect after application of its normal maximum load. This is accomplished by means of an internal bracing system which only comes into operation when maximum deflection has been reached.


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    Title :

    The parker variable camber wing


    Additional title:

    Nat. Advisory Committee Aeronautics, report


    Contributors:


    Publication date :

    1920


    Size :

    41 pages


    Remarks:

    25 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    The Parker Variable Camber Wing

    Parker, H F | NTRS | 1920





    Variable wing area and variable camber

    Irving, H.B. | Engineering Index Backfile | 1920