Unstructured Panel Method Rolling Fixed

Simulation of a

Simulation of a wing-tail configuration with the Aviumtechnologies

Simulation of a

Simulation of a

Simulation of the NREL Phase IV wind turbine with the Aviumtechnologies

Simulation of the Caradonna Tung rotor in hover with the Aviumtechnologies

Simulation of a NACA4412 with the Aviumtechnologies

Lecture 11 is on

Pusan National University Applied Aerodynamic Design Laboratory.

See the paper here: ...

This is part one of two explaining the discrete vortex unsteady

This video shows a simulation's result of a sudden acceleration of a rectangular wing into a constant speed. The aim of the ...

Pusan National University Applied Aerodynamic Design Laboratory.

In the previous video (Building More Complex Flows), we ended with an equation for the velocity potential induced at an arbitrary ...

This is the first real step towards writing a

Illustration of how the coefficient of lift increases as the Kutta condition translates around the Coanda surface. The Kutta condition ...