Author: J. M. Cimbala
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ISBN:
Category :
Languages : en
Pages : 65
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A computer code has been written for a general finite difference solution procedure of the incompressible boundary layer equations on a body of revolution. The procedure, a fourth-order accurate extension of Keller's Box Method, is capable of treating laminar or turbulent boundary layers up to a separation point and includes transverse curvature effects. The analysis has been coded for the Penn State IBM 370/3033 computer and has been shown to provide solutions comparable in accuracy to similar second-order schemes but with fewer grid points and with less computer time. Results and comparisons with both experiment and second-order methods are presented in graphical form for a low-drag body of revolution. (Author).
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ISBN:
Category :
Languages : en
Pages : 32
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 862
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Author: Stephen F. Wornom
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ISBN:
Category : Boundary layer
Languages : en
Pages : 60
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 758
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Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
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Category : Science
Languages : en
Pages : 368
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Author: American Institute of Aeronautics and Astronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages : 436
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Author: Pennsylvania State University
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Category :
Languages : en
Pages : 288
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Author:
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Category : Aeronautics
Languages : en
Pages : 898
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Author: Ward O. Winer, Arthur G. Hansen
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Category :
Languages : en
Pages : 21
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