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Author

Swathi Krishna

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Preprint Aug 2026

A Low-Fidelity Method for Aerofoil Shape Optimisation for Curvilinear Blade Kinematics

This study develops a low-fidelity framework for aerofoil shape optimisation under curvilinear blade kinematics, using a hovering cyclorotor as a representative case. Aerofoil optimisation can improve cyclorotor efficiency by suppressing leading-edge vortex separation during dynamic stall, but conventional approaches r...

Benjamin Irwin, David J. J. Toal, Swathi Krishna · 0 citations

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