A kinesthetic-tactual display may be effectively used as a control aid, per previous flight tests. Angle-of-attack (AOA) information would be continuously presented to a pilot, via this display, during critical operational phases -- approaches to landing, takeoff and departures, and accelerated maneuvers -- where stalls are probable. He would then have a continuous indication of aerodynamic state, and thus perform the necessary control before a stall condition was reached


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    Titel :

    Development of Stall Deterrent Device for Small Airplanes


    Beteiligte:
    R. D. Gilson (Autor:in) / R. W. Fenton (Autor:in)

    Erscheinungsdatum :

    1975


    Format / Umfang :

    66 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    Lachmann, G. | Engineering Index Backfile | 1927


    Development of Stall Deterrent Concepts for General Aviation Aircraft

    H. L. Chevalier / C. R. Gallaway / J. R. Brown | NTIS | 1975


    Investigation of a stall deterrent system utilizing an acoustic stall sensor

    Bennett, A. G. / Owens, J. K. / Harris, R. L. | NTRS | 1977


    Investigation of a Stall Deterrent System Utilizing an Acoustic Stall Sensor

    Bennett, A. G. / Owens, J. K. / Harris, R. L. | SAE Technical Papers | 1977