Design philosophy applied by Louis Breguet Co to improve landing and takeoff speeds; wing of experimental aircraft Br 940 is equipped along its trailing edge with multiple flaps having very steep deflections and exposed to permanent slip-stream of four large propellers placed in front of leading edge; arrangement strongly deflects slipstream downwards and increases lift; as result, landing speed is reduced and speed range improved; aerodynamic problems and tests.


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    Titel :

    STOL aircraft with slipstream boost


    Weitere Titelangaben:

    Aeroplane Astronautics


    Beteiligte:
    Bruner, G. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1959


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :