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jet structure at the end of a 2D supersonic nozzle |
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November 7, 2001, 04:05 |
jet structure at the end of a 2D supersonic nozzle
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I'm using CFX TASCflow to model the 2d jet structure at the exit of a supersonic nozzle. Im having convergence problems using a supersonic inlet condition and a supersonic outlet condition to my flow domain. If any one has any prior experiance in a problem of this nature, your sugegstions will be most welcome
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