boundary conditions for transonic 1d euler

August 4, 2006, 05:30

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??

August 4, 2006, 10:53

Hi,

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 ??)

Dominic

August 4, 2006, 05:30	boundary conditions for transonic 1d euler	#1
Panagis Guest Posts: n/a	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??

August 4, 2006, 10:53	Re: boundary conditions for transonic 1d euler	#2
Dominic Guest Posts: n/a	Hi, 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 ??) Dominic

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