The airplane has a relatively steep spin mode (low angle of attack) with a high load factor and high velocity. The airplane recovers almost immediately after any deviation from the prospin control positions, except for one maneuver with reduced flexibility in the elevator control system.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Spin Tests of a Single-Engine, High-Wing Light Airplane


    Contributors:
    E. C. Stewart (author) / W. T. Suit (author) / T. M. Moul (author) / P. W. Brown (author)

    Publication date :

    1982


    Size :

    93 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Spin tests of a single-engine, high-wing light airplane

    Stewart, E. C. / Suit, W. T. / Moul, T. M. et al. | NTRS | 1982



    Investigations of Modifications to Improve the Spin Resistance of a High-Wing, Single-Engine, Light Airplane

    DiCarlo, D. J. / Manuel, G. S. / Stough, H. P. et al. | SAE Technical Papers | 1989


    High-speed tests of model twin-engine low-wing transport airplane

    Becker, J.V. / Leonard, L.H. | Engineering Index Backfile | 1942


    High-Speed Tests of a Model Twin-Engine Low-Wing Transport Airplane

    Becker, John V / LEONARD LLOYD H | NTRS | 1942