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Solution of the boundary layer over an airfoil section

version 1.0.0.0 (870 KB) by Mohamed Atyya
Solution of the boundary layer over an airfoil section

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Updated 25 Jul 2016

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This code is used to solve the boundary layer over an airfoil section in the three regimes subsonic regime, transition regime and turbulent regime

Comments and Ratings (1)

noe

Updates

1.0.0.0

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MATLAB Release Compatibility
Created with R2013b
Compatible with any release
Platform Compatibility
Windows macOS Linux

Solution of the boundary layer over an airfoil section/