To evaluate relative merits of small and large engines comparison is made of data from different sources confined to engines suitable for Mach number range from 2 to 3 and altitudes of 50,000 to 70,000 ft; favorable cycle characteristics established and feasibility discussed; data, based on Curtiss-Wright Turbomotor Div design activity, show that small turbine engine will inherently satisfy requirements. (see also abstract in Soc Automotive Engrs -- J v 65 n 8 July 1957 p 90-3)


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    Titel :

    Potential advancements in field of small aircraft engines


    Weitere Titelangaben:

    Soc Automotive Engrs -- Paper


    Beteiligte:
    Hensley, R.V. (Autor:in) / Shapiro, S.R. (Autor:in) / Capiaux, R. (Autor:in)

    Kongress:

    Society of Automotive Engineers -- Meeting ; 1957 Small



    Erscheinungsdatum :

    1957


    Format / Umfang :

    20 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    POTENTIAL ADVANCEMENTS IN THE FIELD OF SMALL AIRCRAFT ENGINES

    Capiaux, Raymond / Hensley, Reece V. / Shapiro, Stanley R. | SAE Technical Papers | 1957



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    Webb, W. L. | British Library Online Contents | 1992


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    Advancements in hydrogen expander airbreathing engines

    Glickstein, M.R. / Powell, T.H. | Tema Archiv | 1987