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altitude investigation of performance of turbine-propeller engine and its componentsAn investigation was conducted on a turbine-propeller engine in the NACA Lewis altitude wind tunnel at altitudes from 5000 to 35,000 feet. The applicability of generalized parameters to turbine-propeller engine data, analyses of the compressor, the combustion chambers, and the turbine, and a study of the over-all engine performance are reported. Engine performance data obtained at sea-level static conditions could be used to predict static performance at altitudes up to 35,000 feet by use of the standard generalized parameters.
Document ID
19930086416
Document Type
Other
Authors
Wallner, Lewis E
Saari, Martin J
Date Acquired
August 16, 2013
Publication Date
October 5, 1950
Report/Patent Number
NACA-RM-E50H30
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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