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Dynamic distortion at the exit of a subsonic diffuser of a mixed compression inletMeasuring distortion characteristics at engine face station of axisymmetric inlet
Document ID
19710002736
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kostin, L. C. (North American Rockwell Corp. Los Angeles, CA, United States)
Martin, A. W. (North American Rockwell Corp. Los Angeles, CA, United States)
Millstone, S. D. (North American Rockwell Corp. Los Angeles, CA, United States)
Date Acquired
August 6, 2013
Publication Date
December 1, 1970
Publication Information
Publisher: NASA
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-1644
Report Number: NASA-CR-1644
Accession Number
71N12211
Funding Number(s)
CONTRACT_GRANT: NAS2-4667
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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