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Method of calculating the temperature distributions in the specimen airfoilsAirfoil pressure profile for calculating temperature distributions in simulated turbine blade specimens
Document ID
19670026022
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Bruno, F. L. (Pratt and Whitney Aircraft East Hartford, CT, United States)
Date Acquired
August 3, 2013
Publication Date
July 10, 1967
Subject Category
Structural Mechanics
Accession Number
67N35351
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TURBINE BLADE
TEMPERATURE DISTRIBUTION
AIRFOIL PROFILE
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