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Effect of various diffuser designs on the performance of an experimental turbojet combustor insensitive to radial distortion of inlet airflowEffect of various diffuser designs on performance of experimental turbojet combustor insensitive to radial distortion of inlet airflow
Document ID
19710009086
Document Type
Technical Memorandum (TM)
Authors
Biaglow, J. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1971
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TM-X-2216
E-5975
Accession Number
71N18561
Funding Number(s)
CONTRACT_GRANT: 720-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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