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This document discusses the development of unsteady inviscid flow models for studying the aerodynamics of airfoils, focusing on vortex-sheet formation and the extension of the Kutta condition to unsteady flows. It emphasizes the importance of accurately predicting vortex strength and distribution for effective aerodynamic modeling, particularly in the context of natural flyers and micro aerial vehicles. The proposed vortex-sheet-based model aims to capture both circulation and viscous effects, providing a c

Author

bindushreem261

Language

EN