Tests with Junkers (D 1010) A. 35 type monoplane equipped with sliding weight and water tank to shift position of center of pressure at will; curves show relations between static pressures, elevator settings and throttle positions; computation of required thrust for level flight for each throttle setting with polar of model test as basis; blanketing effect of propeller. From 1930 Yearbook of Deutscher Versuchsanstalt fuer Luftfahrt. (see also Jahrbuch 1930 der Deutschen Versuchsanstalt fuer Luftfahrt, E. V., pp. 49-53, 16 figs.)


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    Title :

    Flight tests for the determination of static longitudinal stability


    Additional title:

    Nat. Advisory Committee Aeronautics -- Tech. Memo


    Contributors:
    Blenk, H. (author)


    Publication date :

    1930


    Size :

    11 pages


    Remarks:

    16 Figs. on Supp. plates


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :