This report treats the following problems: The beginning of the investigated motions is always a setting of the lateral controls, i.e., the rudder or the ailerons. Now, the first interesting question is how the motion would proceed if these settings were kept unchanged for some time; and particularly, what upward motion would set in, how soon, and for how long, since therein lie the dangers of yawing. Two different motions ensue with a high rate of turn and a steep down slope of flight path in both but a marked difference in angle of attack and consequently different character in the resultant aerodynamic forces: one, the "corkscrew" dive at normal angle, and the other, the "spin" at high angle.


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    Titel :

    Combined pitching and yawing motion of airplanes


    Beteiligte:
    Baranoff, A V (Autor:in) / Hopf, L (Autor:in)

    Erscheinungsdatum :

    01.05.1931


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch



    Combined pitching and yawing motion of airplanes

    Von Baranoff, A. / Hopf, L. | Engineering Index Backfile | 1931


    Combined pitching and yawing motion of airplanes

    Baranoff, A. / Hopf, L. | TIBKAT | 1931



    Measurement of dynamic cross-derivatives due to pitching and yawing

    ORLIK-RUECKEMANN, K. / LABERGE, J. / HANFF, E. | AIAA | 1974


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