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Discharge coefficients for thick-plate orificesInvestigation enables more accurate prediction of coolant flows within internally cooled turbine blades and vanes. The data is applicable for predicting flows in complex flow passages.
Document ID
19700000058
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Metger, G. W.
Rhode, J. E.
Richards, H. T.
Date Acquired
August 5, 2013
Publication Date
April 1, 1970
Subject Category
Mechanics
Report/Patent Number
Report Number: LEW-11067
LEW-11067
Accession Number
70B10062
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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