Existing and proposed VTOL test beds examined and their characteristics compared with helicopter requirements on basis of angular acceleration and velocity capability in pitch, roll and yaw; it is found that stability and control requirements of helicopters are applicable; tentative hovering and transition flying qualities for VTOL aircraft should be established using same criteria contained in helicopter specification MIL-H-8501.


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    Titel :

    Hovering and low speed controllability of VTOL aircraft


    Weitere Titelangaben:

    Am Helicopter Soc -- J


    Beteiligte:
    Crim, A.D. (Autor:in)


    Erscheinungsdatum :

    1959


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Effect of stabilization on VTOL aircraft in hovering flight

    Greif, R. K. / Fry, E. B. / Gerdes, R. M. et al. | NTRS | 1972


    Effect of Stabilization on VTOL Aircraft in Hovering Flight

    R. K. Greif / E. B. Fry / R. M. Gerdes et al. | NTIS | 1972