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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    Title :

    Potential advancements in field of small aircraft engines


    Additional title:

    Soc Automotive Engrs -- Paper


    Contributors:
    Hensley, R.V. (author) / Shapiro, S.R. (author) / Capiaux, R. (author)

    Conference:

    Society of Automotive Engineers -- Meeting ; 1957 Small



    Publication date :

    1957


    Size :

    20 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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