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July 25, 1998, 04:14 |
Fluent Code (4.2 V) Limitations
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I am using Fluent Code for my Engineering Project. I am working on compressible fluid(air) for sub-sonic and super-sonic flow. I want to know the maximium Mach No. which can be used and also other limitations of this code. For the case of super-sonic flow the code asked for inlet boundary conditions velocities, static pressure, total temperature and turbulence quantities, would you please guide us with an example the correct use of this boundary condition. (for example for Mach No. 2). Thanks.
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