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Calculation of shear layer length scale for airfoil in deep stall |
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Member
Ravi
Join Date: May 2017
Posts: 32
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Hello all,
I am currently running a DDES, 2nd order unsteady simulation for an airfoil in deep stall (angle of attack (AoA) = ![]() ![]() In order to verify the results obtained from the PSD spectrum of the lift coefficient ![]() Does anyone know of a relationship between the shear layer thickness and airfoil properties, such as chord length and the AoA, or any other formulation? Hoping to hear from you all soon. Last edited by raviramesh10; July 17, 2021 at 09:02. |
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