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Analysis of Total-Pressure Loss and Airflow Distribution for Annular Gas Turbine CombustorsComputer analysis of total pressure loss and air flow distribution in annular flow gas turbine combustion chambers
Document ID
19690023936
Acquisition Source
Headquarters
Document Type
Other - NASA Technical Note (TN)
Authors
Tacina, Robert R. (NASA Lewis Research Center Cleveland, OH, United States)
Grobman, Jack (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1969
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TN-D-5385
Report Number: NASA-TN-D-5385
Accession Number
69N33314
Funding Number(s)
CONTRACT_GRANT: 120-03-00-89-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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