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Heat and mass transfer near the stagnation point when gas is injected or sucked through a body surfaceApproximation method for calculating heat, and mass exchange in laminar multicomponent boundary layer near stagnation point of injected gases
Document ID
19680005177
Acquisition Source
Legacy CDMS
Document Type
Technical Translation (TT)
Authors
Anfimov, N. A. (NASA Headquarters Washington, DC United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1968
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TT-F-11389
Report Number: NASA-TT-F-11389
Accession Number
68N14646
Distribution Limits
Public
Copyright
Public Use Permitted.
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