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April 18, 2005, 11:06
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blunted cone-flare in hypersonic flow
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Guest
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HELLO I am a student of aerospace and i am intersted in CFD. I tryed to solve a hypersonic problem, i found a paperwhich solve somthing like that so I tryed to do like it, i meshed the flowfield but i got a high aspect ratio in some regions from 5 up to 400. please give me an e-mail address to send the pictures of my mesh. then i tryed to solve with fluent coupled implicit with a courant no. about .15 but it diverged after 13000 iterations.(not divergance but instable and the residuals are about 1e-5
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