A two-engine three-fan V/STOL airplane was designed to demonstrate and develop the technology for operational V/STOL and STO-VL aircraft having safe engine-out characteristics. Engine-out requirements, integration of propulsion and aerodynamic controls, and propulsion installation are the major factors affecting the configuration. Use of variable pitch fans enhances the control system providing a responsive and versatile airplane. The ability to operate over the entire flight spectrum from zero speed to M = 0.8 is required to demonstrate operational capability with a V/STOL system.


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    Titel :

    Design of a V/STOL technology airplane


    Beteiligte:
    Zabinsky, J. M. (Autor:in) / Burnham, R. W. (Autor:in)

    Kongress:

    American Institute of Aeronautics and Astronautics, Aircraft Systems and Technology Meeting ; 1975 ; Los Angeles, CA


    Erscheinungsdatum :

    01.08.1975


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Design of a V/STOL technology airplane

    ZABINSKY, J. / BURNHAM, R. | AIAA | 1975


    Design Considerations for a V/STOL Technology Airplane

    Joseph M. Zabinsky / Robert M. Burnham | AIAA | 1976


    Preliminary design of "ARAVA" STOL airplane

    Mankuta, H. / Sa'Ar, D. | Engineering Index Backfile | 1967


    Development of STOL airplane

    MacDonald, A.F. | Engineering Index Backfile | 1960


    V/STOL cargo airplane characteristics

    Garrard, W.C.J. | Engineering Index Backfile | 1961