NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Investigation of the I-40 jet-propulsion engine in the Cleveland altitude wind tunnel III : analysis of turbine performance and effect of tail-pipe design on engine performance
Document ID
19930085419
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Krebs, Richard P
Foshag, Frederick C
Date Acquired
August 29, 2013
Publication Date
August 26, 1948
Report/Patent Number
NACA-RM-E8G02b
Accession Number
93R14709
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