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Gas side heat transferImprovements in methods for predicting heat transfer rates on the hot gas side of turbine airfoils are necessary for improved turbine durability and performance. The development and verification of improved analytical models requires a systematic, closely coupled experimental and analytical program.
Document ID
19860002040
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hylton, L. D. (Detroit Diesel Allison MI, United States)
Date Acquired
August 12, 2013
Publication Date
October 1, 1983
Publication Information
Publication: NASA. Lewis Research Center Turbine Eng. Hot Sect. Technol. (HOST)
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
86N11507
Funding Number(s)
CONTRACT_GRANT: NAS3-23695
CONTRACT_GRANT: NAS3-22761
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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