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Thermal feasibility of using methane or hydrogen fuel for direct cooling of a first-stage turbine-statorMethane or hydrogen fuel direct cooling of first stage stator of SST aircraft turbine - numerical heat transfer analysis
Document ID
19700033010
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Colladay, R. S. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1970
Subject Category
Thermodynamics And Combustion
Report/Patent Number
E-5701
NASA-TN-D-6042
Accession Number
70N42326
Funding Number(s)
CONTRACT_GRANT: 720-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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