TAGGED: around-the-cylinder, cfd-convergence, cfd-fluent, hypersonic
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September 6, 2021 at 4:58 am
Cephied
SubscriberHello,
I am running a simulation of a half cylinder in a hyper-sonic flow. My goal is to resolve the heat flux along the boundary of the cylinder wall. Consider this case to be a hollow cylinder. A contour of the mach number is given here for visualization of the problem. The simulation has ran for a total of 40K iterations at the time of this post.
September 6, 2021 at 10:29 amRob
Forum ModeratorCheck the flux result every some iterations, you may have a transient effect in the system.
Why are you including volumetric reactions? Unless you're going to be reacting the air I'd just use "air" to save on cpu load.
September 6, 2021 at 6:28 pmCephied
SubscriberThank you for the reply! Volumetric reactions are included because they are necessary for our goals with the simulation. Currently I am trying to resolve the heat-flux on the wall boundary, but this is only a PART of the total goal for this project.
When you say transient effect...do you mean that the simulation has yet to reach steady-state (AKA run longer)?
September 7, 2021 at 6:06 amDrAmine
Ansys EmployeeYou might turn on Two-Temperature Model for Hypersonic Flows. Regarding the noise: that might be an indicator of unsteadiness. You might run unsteady or turn data sampling for steady state. There are some more way's to remove noise when it comes to heat transfer (only pressure based).
Viewing 3 reply threads- The topic ‘Numerical Stability Issues with Surface Heat Flux Along Hollow Cylinder Wall’ is closed to new replies.
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