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Evaluation of circumferential airflow uniformity entering combustors from compressors. Volume 2: Data supplementA study of the airflow uniformity leaving compressors and entering combustors was made using compressors from two advanced engines, the J58 and F100/F401. The data used in the analysis of each case is presented in tabular form and computer-generated profile plots. A plot of the square root of the dynamic pressure ratio, which is similar to airflow deviation, is also presented.
Document ID
19730005550
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Shadowen, J. H.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Egan, W. J., Jr.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1972
Subject Category
Fluid Mechanics
Report/Patent Number
PWA-FR-5183-VOL-2
NASA-CR-121010
Report Number: PWA-FR-5183-VOL-2
Report Number: NASA-CR-121010
Accession Number
73N14277
Funding Number(s)
CONTRACT_GRANT: NAS3-15693
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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