Lift tailoring on unsteady airfoils with leading-edge vortex shedding using an inverse aerodynamic approach
In this paper, we present a physics-informed approach to tailor the lift profile of an unsteady
airfoil through the execution of an appropriate maneuver. In previous research, a low-order …
airfoil through the execution of an appropriate maneuver. In previous research, a low-order …
Effect of Rounded Trailing Edges on Unsteady Airfoil Loading at Low Reynolds Numbers
The steady potential flow past a traditional airfoil with a round leading edge and a sharp
trailing edge can usually be simulated using the assumption of Kutta condition at the trailing …
trailing edge can usually be simulated using the assumption of Kutta condition at the trailing …