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Supersonic variable-cycle enginesThe evolution and current status of selected recent variable cycle engine (VCE) studies are reviewed, and how the results were influenced by airplane requirements is described. Promising VCE concepts are described, their designs are simplified and the potential benefits in terms of aircraft performance are identified. 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, ongoing technology programs in acoustics and exhaust emissions is also presented. 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
19770003117
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Willis, E. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Welliver, A. D.
(Boeing Aerospace Co. Seattle, Wash., United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1976
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-X-73524
Report Number: NASA-TM-X-73524
Meeting Information
Meeting: Propulsion Conf.
Location: Palo Alto, CA
Country: United States
Start Date: July 26, 1976
End Date: July 29, 1976
Sponsors: AIAA, SAE
Accession Number
77N10059
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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