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NASA NTRS ยท 19830013933

Energy efficient engine component development and integration program

Abstract

The technology that will improve the energy efficiency of propulsion systems for subsonic commercial aircraft is investigated. A reduction of 14.4% in cruise installed sfc (0.572 versus 0.668 for the CF6-50C) and a direct operation cost reduction in excess of the 5% goal is projected. Noise and emissions projections are consistent with the established goals.

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BibTeXRIS

1981-01-30. Energy efficient engine component development and integration program. https://ntrs.nasa.gov/citations/19830013933

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