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Engine investigation of an impingement-cooled turbine rotor bladeExperimentally determined heat transfer characteristics of an impingement-cooled turbine rotor blade are reported. The test results are compared with those obtained for three convection-cooled turbine blades tested in the same facility in addition to impingement correlations found in literature.
Document ID
19730016202
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Gauntner, J. W. (NASA Lewis Research Center Cleveland, OH, United States)
Livingood, J. N. B. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1973
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TM-X-2791
E-7313
Report Number: NASA-TM-X-2791
Report Number: E-7313
Accession Number
73N24929
Funding Number(s)
PROJECT: RTOP 501-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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