NASA Logo

NTRS

NTRS - NASA Technical Reports Server

The auto‑search feature has been disabled based on user feedback. Enter a search term/phrase and click “Search” to begin.

Back to Results
Analysis of limitations imposed on one-spool turbojet-engine designs by compressors and turbines at flight Mach numbers of 0, 2.0, and 2.8
Document ID
19930088284
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Cavicchi, Richard H
English, Robert E
Date Acquired
August 29, 2013
Publication Date
September 24, 1954
Report/Patent Number
NACA-RM-E54F21a
Report Number: NACA-RM-E54F21a
Accession Number
93R17574
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available