A Design Method for Entrance Sections of Transonic Wind Tunnels with Rectangular Cross Sections
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Page : 40 pages
File Size : 38,75 MB
Release : 1975
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Page : 40 pages
File Size : 38,75 MB
Release : 1975
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Page : 704 pages
File Size : 30,82 MB
Release : 1995
Category : Aeronautics
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Page : 44 pages
File Size : 50,57 MB
Release : 1979
Category : Computer programs
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Page : 444 pages
File Size : 25,36 MB
Release : 1987
Category : Computer software
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Author : James D. Keller
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Page : 26 pages
File Size : 28,28 MB
Release : 1971
Category : Boundary layer
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A numerical method is presented for calculating the boundary-induced interference at subsonic speeds in wind tunnels of rectangular cross section with slotted or perforated walls. The slot width or wall porosity can vary throughout the test section. The interference can be computed at any point in the test section. The model can be any configuration and can be located anywhere in the test section. Several examples are given, and comparison is made with other methods were available.
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Page : 934 pages
File Size : 41,8 MB
Release : 1948
Category : Mechanics, Applied
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Page : 972 pages
File Size : 47,72 MB
Release : 1982-03
Category : Science
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Author : United States. National Aeronautics and Space Administration. Computer Software Management and Information Center
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Page : 484 pages
File Size : 23,88 MB
Release : 1993
Category : Computer software
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Author : George M. Stokes
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Page : 60 pages
File Size : 44,67 MB
Release : 1956
Category : Boundary layer
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Publisher : Elsevier Publishing Company
Page : 574 pages
File Size : 27,23 MB
Release : 1985
Category : Science
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