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Supersonic flow over a flat plate and a blunt body. |
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August 31, 2010, 17:35 |
Supersonic flow over a flat plate and a blunt body.
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Shushank Ravi Arora
Join Date: Aug 2010
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Hi everyone,
I have to do a flow over a flat plate as well as blunt body. i am planning to run the above for three different Mach numbers 2,3 and 4. i have to concentrate on the boundary layer generated over these bodies. The following parameters are to be compared with experimental results - Skin friction coefficient, Mach number, momentum thickness, displacement thickness, boundary layer thickness, shock strength and separation length. How to i do this using fluent? Where do i get the data from and how do i validate it? looking forward to results Thank you all in advance |
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