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boundary conditions for transonic 1d euler

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Old   August 4, 2006, 04:30
Default boundary conditions for transonic 1d euler
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I am trying to run a transonic case in my adjoint optimization program for my thesis. Till now I can run subsonic problems and the results are ok. However I can't find the appropriate boundary conditions needed for the transonic problem. At the inlet of the duct H and po must be determined and at the throat the mach should be 1. But something is missing. any help??
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Old   August 4, 2006, 09:53
Default Re: boundary conditions for transonic 1d euler
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What is your test case in specific ? like whats that your testing actually ? you can refer to Anderson for a deep insight on a Nozzle problem(Is it a nozzle ??)


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