Theoretical analysts of lateral dynamic motion of tailless and conventional airplanes was made for fighter and heavy transport. Their reactions to a lateral gust and control power required by each for simple maneuvers were determined and compared. Both types of airplanes require almost identical aileron control power to perform a given maneuver; tailless airplane requires about 1-2 to 1-3 directional control power of conventional airplane. Tailless airplane also shows greatest displacement for a given disturbance and has least damping in oscillatory mode.


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    Titel :

    A Comparison of the Lateral Motion Calculated for Tailless and Conventional Airplanes


    Beteiligte:

    Erscheinungsdatum :

    1947-02-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Comparison of lateral motion calculated for tailless and conventional airplanes

    Harper, C.W. / Jones, A.L. | Engineering Index Backfile | 1947



    Generalized performance comparison of large conventional, tail-boom, and tailless airplanes

    Ankenbruck, H.O. / McKinney, Jr., M.O. | Engineering Index Backfile | 1947



    Wing tips for tailless airplanes

    Weyl, A.R. | Engineering Index Backfile | 1945