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Single stage experimental evaluation of variable geometry guide vanes and stator blading. Part 3 - Data and performance for variable camber guide vane and stator APerformance tests of variable camber guide vane and stator to extend range of axial flow compressors
Document ID
19690004677
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Jones, B. A. (Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Oscarson, R. P. (Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Date Acquired
August 5, 2013
Publication Date
December 4, 1968
Subject Category
Aerodynamics
Report/Patent Number
PWA-FR-2638-PT-3
NASA-CR-54556
Report Number: PWA-FR-2638-PT-3
Report Number: NASA-CR-54556
Accession Number
69N14009
Funding Number(s)
CONTRACT_GRANT: NAS3-7604
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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