NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
A thermodynamic study of the turbine-propeller engineEquations and charts are presented for computing the thrust, the power output, the fuel consumption, and other performance parameters of a turbine-propeller engine for any given set of operating conditions and component efficiencies. Included are the effects of the pressure losses in the inlet duct and the combustion chamber, the variation of the physical properties of the gas as it passes through the system, and the change in mass flow of the gas by the addition of fuel.
Document ID
19930092150
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Pinkel, Benjamin
Karp, Irvin M
Date Acquired
September 6, 2013
Publication Date
January 1, 1953
Report/Patent Number
NACA-TR-1114
Accession Number
93R21440
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitleNACA-TN-2653Superseded By
No Preview Available