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Get the solution in the exhaust jet #2

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xavierdechamps opened this issue Sep 9, 2019 · 1 comment
Open

Get the solution in the exhaust jet #2

xavierdechamps opened this issue Sep 9, 2019 · 1 comment
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enhancement New feature or request

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Apply the free pressure boundary point.
Verify if static pressure at nozzle exit lip point exceeds the stagnation pressure (then expansion wave) or is less than the stagnation pressure (oblique shock wave).
@xavierdechamps xavierdechamps added the enhancement New feature or request label Sep 9, 2019
@xavierdechamps xavierdechamps self-assigned this Sep 9, 2019
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xavierdechamps commented Sep 24, 2019 •
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Partially improved the flow field inside the plume: only the under-expanded nozzle is considered for the moment, where a Prandtl-Meyer expansion fan appears at the exit of the nozzle. Commit 3ac0b79 brought this modification. Over-expanded nozzle still to be done.

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