The aerodynamic effectiveness of various propulsive lift concepts to provide for the low speed performance and control required for short takeoff and landing aircraft is discussed. The importance of the interrelationship between the propulsion system and aerodynamic components of the aircraft is stressed. The relative effectiveness of different lift concepts was evaluated through static and wind tunnel tests of various aerodynamic models and propulsion components, simulations of aircraft, and in some cases, flight testing of research aircraft incorporating the concepts under study. Results of large scale tests of lift augmentation devices are presented. The results of flight tests of STOL research aircraft with augmented jet flaps and rotating cylinder flaps are presented to show the steeper approach flight paths at low forward speeds.


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    Titel :

    Aerodynamics of jet flap and rotating cylinder flap STOL concepts


    Beteiligte:
    Cook, W. L. (Autor:in) / Hickey, D. H. (Autor:in) / Quigley, H. C. (Autor:in)


    Erscheinungsdatum :

    1974-10-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Aerodynamics of the Gurney flap

    Jeffrey, David / Hurst, David | AIAA | 1996




    Blown flap system for STOL performance -- Weight considerations

    Schwartzberg, M. | Engineering Index Backfile | 1959


    V/STOL aerodynamics

    Tema Archiv | 1975