NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Effect of sweep on performance of compressor blade sections as indicated by swept-blade rotor, unswept-blade rotor, and cascade tests
Document ID
19930084940
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Godwin, William R
Date Acquired
August 16, 2013
Publication Date
July 1, 1957
Report/Patent Number
NACA-TN-4062
Report Number: NACA-TN-4062
Accession Number
93R14230
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available