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Old   May 16, 2005, 17:53
Default Supersonic nozzle
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Danny Tan
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Dear CFD people:

Is it possible to obtain uniform, isentropic, shock free flow through a minimum length nozzle (MLN), (the expansion section is eliminated) ?

I believe it is possible but..

My question is: If it is possible to obtain uniform, isentropic, shock free flow through MLN, why people want to design a long supersonic nozzle with gently curved expansion section.

Any comment is appreciated

Thank you

Danny
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