Study develops accurate and easily calculated results from method of analysis perfected by author; its accuracy is enhanced by analyzing flight test results obtained from Breguet 941, deflected slipstream S TOL aircraft; method solves problem of calculating transitional velocities, of climb, takeoff, and landing distances with highly deflected flaps; mathematical calculations and charts illustrate results of computations and comparison with flight test data; interesting aspect of Breguet 941 is very high static thrust of 18,000 lb developed by four propellers.


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    Titel :

    Determination of breguet 941 STOL aircraft transition velocities with various flap deflections


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Fowler, H.D. (Autor:in)

    Kongress:

    SAE Meeting ; 1965 VTOL-STOL



    Erscheinungsdatum :

    1965


    Format / Umfang :

    26 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Breguet family of STOL aircraft

    Ricard, G. / Czinczenheim, J. / Jaillard, P.E. et al. | Engineering Index Backfile | 1961


    Breguet family of STOL aircraft

    Ricard, G. / Czinczenheim, J. / Jaillard, P.E. et al. | Engineering Index Backfile | 1961


    The Breguet Family of STOL Aircraft

    Ricard, Georges / de Richemont, Guy / Czinczenheim, Joseph et al. | SAE Technical Papers | 1961