NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Investigation of Impulse-type Supersonic Compressor with Hub-tip Ratio of 0.6 and Turning to Axial Direction I : Performance of Rotor Alone
Document ID
19930088163
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Wilcox, Ward W
Date Acquired
August 16, 2013
Publication Date
May 6, 1954
Report/Patent Number
NACA-RM-E54B25
Report Number: NACA-RM-E54B25
Accession Number
93R17453
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available