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Performance of short length turbojet combustor insensitive to radial distortion of inlet airflowPerformance of short length turbojet combustor insensitive to radial distortion of inlet airflow
Document ID
19700008821
Document Type
Other - NASA Technical Note (TN)
Authors
Humenik, F. M. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1970
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TN-D-5570
E-5176
Accession Number
70N18126
Funding Number(s)
CONTRACT_GRANT: 720-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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