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.
Application of regenerative engines to current and future aircraft
SAE -- Paper
SAE Meeting ; 1965 Regenerators
1965
9 pages
Aufsatz (Konferenz)
Englisch
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Application of Regenerative Engines to Current and Future Aircraft
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