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)