How to set transition location
I have a ploblem concerning flow over an airfoil. Lift characteristics are pretty good, but drag - no. Therefore I want to know how to set transition point in boundary layer in star-cd for more proper results. How to force star-cd use laminar algorithm in one part of BL and one of turbulent algorithms in another?
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Re: How to set transition location
The code has no transition modeling available. For details, ask Sheila in this forum. Sorry...
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Re: How to set transition location
I don't need modelling. What if I to want to set this point by myself and star-cd will treat one part of BL before this point as laminar BL and another, after this point as turbulent? How can I ask Sheila? This is forum, not chat.
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Re: How to set transition location
By email:)
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