A combined CFD, wind tunnel and neural network analysis shows trailing-edge serrations raise stall angles on NACA 0012 ...
A controlled CFD comparison found NACA 2412 had the highest lift-to-drag ratio among five NACA 24-series airfoils, while a ...
“Zero-thickness” designs of airfoils to minimize drag or maximize lift. Evolutionary algorithms have shown that designs which have the least drag have a strongly corrugated shape (top), while those ...
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