Calculation of turbulent boundary layers with heat transfer and pressure gradient utilizing a compressibility transformation. Part III, Computer program manual / by J. Schneider and J. Boccio.

A computer program is described capable of determining the properties of a compressible turbulent boundary layer with pressure gradient and heat transfer. The program treats the two-dimensional problem assuming perfect gas and Crocco integral energy solution. A compressibility transformation is appl...

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Online Access: Search for the full-text version of this title in HathiTrust
Main Author: Schneider, J.
Corporate Authors: General Applied Science Laboratories (Westbury, Nassau County, N.Y.), Langley Research Center, United States. National Aeronautics and Space Administration
Other Authors: Boccio, J.
Format: Government Document Book
Language:English
Published: Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service [distributor], 1972.
Series:NASA contractor report ; NASA CR-1925.
Subjects:

MARC

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520 |a A computer program is described capable of determining the properties of a compressible turbulent boundary layer with pressure gradient and heat transfer. The program treats the two-dimensional problem assuming perfect gas and Crocco integral energy solution. A compressibility transformation is applied to the equation for the conservation of mass and momentum, which relates this flow to a low speed constant property flow with simultaneous mass transfer and pressure gradient. The resulting system of describing equations consists of eight ordinary differential equations which are solved numerically. For Part 1, see N72-12226; for Part 2, see N72-15264. 
536 |a Performed by General Applied Science Laboratories, Inc., Westbury, L.I., New York, for Langley Research Center  |b NAS1-9624. 
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