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Single stage experimental evaluation of variable geometry inlet guide vanes and stator blading, part 6 Final reportVariable geometry inlet guide vanes and stators for extending stable operation of supersonic cruise turbine engine compressor front stage
Document ID
19700014098
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Jones, B. A. (Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Date Acquired
August 5, 2013
Publication Date
March 15, 1970
Subject Category
Propulsion Systems
Report/Patent Number
PWA-FR-2641
NASA-CR-54559
Report Number: PWA-FR-2641
Report Number: NASA-CR-54559
Accession Number
70N23403
Funding Number(s)
CONTRACT_GRANT: NAS3-7604
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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