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How to compute a value in the wall normal direction?

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Old   October 29, 2015, 11:39
Default How to compute a value in the wall normal direction?
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how can I compute in streamwise direction (along the airfoil surface), the distance in the wall-normal direction (practically the distance from the airfoil surface) above which a certain value is exceeded (e.g. a value F becomes > 1)?

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