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 Nat. Advisory Committee Aeronautics -- Tech. Memo., no. 584, Sept. 1930, 11 pp., 16 figs. on supp. plates)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Flight tests for the determination of static longitudinal stability


    Additional title:

    Jahrbuch 1930 der Deutschen Versuchsanstalt fuer Luftfahrt, E. V.


    Contributors:
    Blenk, H. (author)


    Publication date :

    1930


    Size :

    5 pages


    Remarks:

    16 figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Flight tests for the determination of static longitudinal stability

    Blenk, H. | Engineering Index Backfile | 1930




    Civil helicopter instrument longitudinal static stability verification flight test method

    QIN CHONG / DONG SHENGHUA / XU CHAOLIANG et al. | European Patent Office | 2025

    Free access

    Aeroelastic Characteristics and Static Stability of Hang Gliders in Longitudinal Flight

    Altmann, H. | British Library Conference Proceedings | 1994