NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Compressor and Turbine MatchingCompressor and gas turbine engine matching - power turbine, turbojet, and turboprop engines
Document ID
19650013761
Acquisition Source
Glenn Research Center
Document Type
Other
Authors
James F Dugan Jr (Glenn Research Center Cleveland, United States)
Date Acquired
August 2, 2013
Publication Date
January 1, 1965
Subject Category
Aerodynamics
Accession Number
65N23362
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
GAS TURBINE
TURBINE ENGINE
AXIAL FLOW COMPRESSOR
Document Inquiry

Available Downloads

There are no available downloads for this record.

Related Records

IDRelationTitle19650013744Collected WorksAerodynamic Design of Axial Flow Compressors19650013744Collected WorksAerodynamic Design of Axial Flow Compressors
No Preview Available