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Variable-cycle engines for supersonic cruising aircraftThe paper reviews the evolution and current status of selected recent variable-cycle engine (VCE) studies and describes how the results are influenced by airplane requirements. The engine/airplane studies are intended to identify promising VCE concepts, simplify their designs and identify the potential benefits in terms of aircraft performance. This includes range, noise, emissions, and the time and effort it may require to ensure technical readiness of sufficient depth to satisfy reasonable economic, performance, and environmental constraints. A brief overview of closely-related, on-going technology programs in acoustics and exhaust emissions is presented. It is shown that realistic technology advancements in critical areas combined with well matched aircraft and selected VCE concepts can lead to significantly improved economic and environmental performance relative to first-generation SST predictions.
Document ID
19760059444
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Willis, E. A.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Welliver, A. D.
(Boeing Aerospace Co. Seattle, Wash., United States)
Date Acquired
August 8, 2013
Publication Date
July 1, 1976
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 76-759
Meeting Information
Meeting: Propulsion Conference
Location: Palo Alto, CA
Start Date: July 26, 1976
End Date: July 29, 1976
Sponsors: American Institute of Aeronautics and Astronautics and Society of Automotive Engineers
Accession Number
76A42410
Distribution Limits
Public
Copyright
Other

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