NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Effect of rotor tip clearance on the performance of a 5-inch single stage axial flow turbineEffect of rotor tip clearance on performance of 5-inch single-stage axial flow turbine
Document ID
19690011521
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Futral, S. M., Jr. (NASA Lewis Research Center Cleveland, OH, United States)
Holeski, D. E. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1969
Subject Category
Auxiliary Systems
Report/Patent Number
NASA-TM-X-1757
Report Number: NASA-TM-X-1757
Accession Number
69N20883
Funding Number(s)
CONTRACT_GRANT: 120-27-03-13-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

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