Multi-engine airplanes divided into those which can and those which cannot fly with full normal load after one or more engines have stopped; ability to fly with one engine necessitates sacrifice in pay-load; insurance against forced landings gained only at cost of increased fuel consumption and greater head resistance; propeller speed less with dead engine; turning forces on plane present problem; single-engine plane has longer range. (See also - discussion p 192-194)


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    Titel :

    Single-engine versus multi-engine airplanes


    Weitere Titelangaben:

    Soc. Automotive Engrs. -- Jl


    Beteiligte:
    Fokker, A.H.G. (Autor:in)


    Erscheinungsdatum :

    1928


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Single-Engine versus Multi-Engine Airplanes

    FOKKER, A. H. G. | SAE Technical Papers | 1928


    Multi-engine airplanes and forced landings

    Smith, H.G. | Engineering Index Backfile | 1926


    Electronic turbo regulator for multi-engine airplanes

    Gille, W.H. / Sparrow, H.T. | Engineering Index Backfile | 1944


    Electronic turbo regulator for multi-engine airplanes

    Gille, W.H. / Sparrow, H.T. | Engineering Index Backfile | 1944


    Electronic turbo regulator for multi-engine airplanes

    Gille, W.H. / Sparrow, H.T. | Engineering Index Backfile | 1944