Tests in Langley 19-ft pressure tunnel of 0.2375-scale model of Douglas XA-26 airplane compared with these measured in flight tests of Douglas A-26B airplane. (released 1948) (15¢)


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    Title :

    Comparison of wind-tunnel and flight measurements of stability and control characteristics of Douglas A-26 airplane


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:
    Kayten, G.G. (author) / Koven, W. (author)


    Publication date :

    1945


    Size :

    14 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :