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Evaluation of circumferential airflow uniformity entering combustors from compressors. Volume 2 : Data supplement

Author
Egan, W. J., Jr.
Published
Nov 1, 1972.
Physical Description
1 electronic document
Additional Creators
Shadowen, J. H.
Online Version

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
A 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.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19730005550.
Accession ID: 73N14277.
NASA-CR-121010.
PWA-FR-5183-VOL-2.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15944570