A progressive symbolic regression framework discovers an interpretable analytical formula chain for skin friction prediction across subsonic to hypersonic attached flows using inviscid surface flow features.
Numerical evaluation of airfoil friction drag.Journal of aircraft, 37(2):354–356, 2000
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Skin friction prediction for attached flows based on two-dimensional inviscid solutions
A progressive symbolic regression framework discovers an interpretable analytical formula chain for skin friction prediction across subsonic to hypersonic attached flows using inviscid surface flow features.