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CASCADE INVESTIGATION OF COOLING CHARACTERISTICS OF A CASTFINNED AIR-COOLED TURBINE BLADE FOR USE IN A TURBOPROP ENGINECascade investigation of cooling characteristics of air-cooled turbine blade for use in turboprop engine
Document ID
19630002637
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Hickel, R. O. (NASA Lewis Research Center Cleveland, OH, United States)
Richards, H. T. (NASA Lewis Research Center Cleveland, OH, United States)
Stepka, F. S. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
June 12, 1957
Subject Category
Propellants
Report/Patent Number
NACA-RM-E57D19
Accession Number
63N12513
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
COOLING
TURBINE BLADE
AIR COOLING
GAS FLOW
TURBOPROP ENGINE
CASCADE

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