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Linearized Theory of Stagnation Point Heat and Mass Transfer at Hypersonic SpeedsSolution for shock layer energy equation with mass and convective heat transfer at hypersonic speed
Document ID
19690024043
Acquisition Source
Headquarters
Document Type
Other - NASA Technical Note (TN)
Authors
Yoshikawa, Kenneth K. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1969
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-5246
Report Number: NASA-TN-D-5246
Accession Number
69N33421
Funding Number(s)
CONTRACT_GRANT: 129-01-02-05-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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