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