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Engine design considerations for 2nd generation supersonic transportsThe environmental and economic goals projected for advanced supersonic transports will require revolutionary improvements in propulsion systems. Variable cycle engine concepts that incorporate unique components and advanced technologies show promise in meeting these goals. Pratt & Whitney Aircraft is conducting conceptual design studies of variable cycle engine concepts under NASA sponsorship. This paper reviews some of the design considerations for these engine concepts. Emphasis is placed on jet noise abatement, reduction of emissions, performance improvements, installation considerations, hot-section characteristics and control system requirements. Two representative variable cycle engine concepts that incorporate these basic design considerations are described.
Document ID
19750056458
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Howlett, R. A.
(United Aircraft Corp. Pratt and Whitney Aircraft Div., East Hartford, Conn., United States)
Date Acquired
August 8, 2013
Publication Date
May 1, 1975
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
SAE PAPER 750628
Meeting Information
Meeting: Society of Automotive Engineers, Air Transportation Meeting
Location: Hartford, CT
Start Date: May 6, 1975
End Date: May 8, 1975
Sponsors: Society of Automotive Engineers
Accession Number
75A40530
Distribution Limits
Public
Copyright
Other

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