Possibility of improving aircraft range, payload, and endurance through application of regenerative cycle engines is examined; paper covers turboshaft, turboprop, and turbofan engines (over bypass ratio range of 0 to 9) of regenerative and nonregenerative types; engine weight and performance estimates are projected through first and second generation developments which are estimated to transpire in 1970-1980 time period; analysis provides trend of relative improvement of regenerative cycle engines with respect to nonregenerative engines.


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    Title :

    Application of regenerative engines to current and future aircraft


    Additional title:

    SAE -- Paper


    Contributors:
    Sallee, G.P. (author) / Mehwald, G. (author)

    Conference:

    SAE Meeting ; 1965 Regenerators



    Publication date :

    1965


    Size :

    9 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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