NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Effect of stage spacing on performance of 3.75-inch-mean-diameter two-stage turbine having partial admission in the first stageStage spacing effect on performance of two-stage turbine with partial admission in first stage
Document ID
19640011358
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Nusbaum, W. J. (NASA Lewis Research Center Cleveland, OH, United States)
Wong, R. Y. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1964
Subject Category
Propellants
Report/Patent Number
NASA-TN-D-2335
Report Number: NASA-TN-D-2335
Accession Number
64N21272
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TWO-STAGE TURBINE

Related Records

There are no records associated with this record.
No Preview Available