Aerodynamic Flight Test Results for the Adaptive Compliant Trailing Edge (AIAA 2016-3855)
Aeroelastic numerical approach of a wing based on the finite element and boundary element methods
Aeroelastic numerical approach of a wing based on the finite element and boundary element methods
AIAA-2003-4065 Experimental Investigation of the Flowfield of a Symmetrical Airfoil in Ground Effect
Aircraft design cycle time reduction using artificial intelligence
Aircraft design cycle time reduction using artificial intelligence
Alternative approaches to preservation of paved road infrastructure