Tests in N.A.C.A. full-scale wind tunnel to determine effect of retractable landing-gear openings in bottom surface of wing upon take-off characteristics of Lockheed Altair airplane; determination of lift and drag characteristics throughout angle-of-attack range with landing gear both retracted and extended.


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    Title :

    Aerodynamic effect of retractable landing gear


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Notes


    Contributors:


    Publication date :

    1933


    Size :

    3 pages


    Remarks:

    3 Supp sheets


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :





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