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Cold-air investigation of effects of partial admission on performance of 3.75-inch mean-diameter single stage axial-flow turbinePartial admission operation effects on performance of single stage axial flow turbine
Document ID
19680020769
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Klassen, H. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1968
Subject Category
Auxiliary Systems
Report/Patent Number
E-4407
NASA-TN-D-4700
Report Number: E-4407
Report Number: NASA-TN-D-4700
Accession Number
68N30241
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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