Direct Simulation of Flight Stability

The New Theory of Flight based on computational solution of the Navier-Stokes equations with slip boundary condition allows direct simulation of dynamic flight stability under the action of aileron, rudder and elevator using the Fluid-Structure-Interaction code Unicorn/FEniCS. This is a new capability which opens many possibilities of new design and control.

AIAA says no-thanks to this capability when rejecting the New Theory of Flight. It is not so clever. Compare Flapping Bird.