Test results indicate: (1) by decreasing fabric deflection between pressure ribs, span load distribution was considerably modified near center and wing moment relations were changed; and (2) minimum drag was less for idling propeller than for propeller locked in vertical position.


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    Title :

    Flight and wind-tunnel tests of XBM-1 dive bomber


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Donely, P. (author) / Pearson, H.A. (author)


    Publication date :

    1938


    Size :

    18 pages


    Remarks:

    22 Supp plates, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Flight and wind-tunnel tests of XBM-1 dive bomber

    Donely, P. / Pearson, H.A. | Engineering Index Backfile | 1938


    Flight and Wind-tunnel Tests of an XBM-1 Dive Bomber

    Donely, Philip / Pearson, Henry A | NTRS | 1938


    Building dive bomber

    Engineering Index Backfile | 1943


    Germany's dive-bomber

    Engineering Index Backfile | 1940


    1,700 H.P. dive bomber

    Engineering Index Backfile | 1942