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Calculations of economy of 18-cylinder radial aircraft engine with exhaust-gas turbine geared to the crankshaftCalculations based on dynamometer test-stand data obtained on an 18-cylinder radial engine were made to determine the improvement in fuel consumption that can be obtained at various altitudes by gearing an exhaust-gas turbine to the engine crankshaft in order to increase the engine-shaft work.
Document ID
19930091900
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Hannum, Richard W
Zimmerman, Richard H
Date Acquired
September 6, 2013
Publication Date
January 1, 1945
Report/Patent Number
NACA-TR-822
Report Number: NACA-TR-822
Accession Number
93R21190
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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