All factors exclusive of reliability can be evaluated so as to provide good basis for choosing engine; effect of changes in engine weight on operating cost; tables show effect of increased engine weight, operating cost, and operation-expense items that are affected; increasing weight of 200-hp. engine from 400 to 494 lb. would be justified provided increases in time between partial and major overhauls and total life could be correspondingly increased; engine resistance. (See also - discussion p 224-225)


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    Titel :

    Gaging airplane-engine performance


    Weitere Titelangaben:

    Soc. Automotive Engrs. -- Jl


    Beteiligte:
    Geisse, J.H. (Autor:in)


    Erscheinungsdatum :

    1930


    Format / Umfang :

    4 pages


    Anmerkungen:

    1 Fig.


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Gaging Airplane-Engine Performance

    GEISSE, J. H. | SAE Technical Papers | 1930


    Factors of airplane engine performance

    Gage, Victor R | NTRS | 1921


    Airplane performance determined by engine performance

    Upton, G.B. | Engineering Index Backfile | 1918


    FUEL GAGING SYSTEM ACCURACIES

    SAE Technical Papers | 1973


    Low-G Propellant Gaging

    G. Orton | NTIS | 1987