An Investigation of the High Speed Turbulent Boundary Layer with Heat Transfer and Arbitrary Pressure Gradient. Part 3 - Computer Program Manual PDF Download
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Languages : en
Pages : 100
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Category :
Languages : en
Pages : 100
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Category : Aeronautics
Languages : en
Pages : 324
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Category : Government publications
Languages : en
Pages : 1730
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Category :
Languages : en
Pages : 110
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Category : Science
Languages : en
Pages : 922
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Author: J. Schneider
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Category : Boundary layer
Languages : en
Pages : 106
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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.
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Category : Science
Languages : en
Pages : 900
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Author: United States. National Technical Information Service
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Category : Computer programs
Languages : en
Pages : 336
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![Documentation of Plasma Physics. Pt. 1, Experimental Plasma Physics [and] Theoretical Plasma Physics PDF](https://books.google.com/books/content/images/frontcover/7gwwAQAAIAAJ?fife=w80-h100)
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Category : Plasma (Ionized gases)
Languages : en
Pages : 582
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Category : Cosmic physics
Languages : en
Pages : 1190
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