Generic Lambda Wing Configuration in Compressible Flow: Effect of Highly Integrated Intakes
Generic Lambda Wing Configuration in Compressible Flow: Effect of Highly Integrated Intakes
Boundary-layer transition measurements on Mach-scaled helicopter rotor blades in climb
Boundary-layer transition measurements on Mach-scaled helicopter rotor blades in climb
Dynamic Stall Simulations on a Pitching Finite Wing (AIAA 2016-4166)
Dynamic Stall Simulations on a Pitching Finite Wing
Dynamic Stall Simulations on a Pitching Finite Wing
Detection of Unsteady Boundary Layer Transition Using Three Experimental Methods (AIAA 2016-1072)
On the Effect of Rotational Forces on Rotor Blade Boundary-Layer Transition (AIAA 2018-0309)