Supersonic flow over a flat plate and a blunt body.
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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