Generic Lambda Wing Configuration in Compressible Flow: Effect of Highly Integrated Intakes
Generic Lambda Wing Configuration in Compressible Flow: Effect of Highly Integrated Intakes
Investigations of dynamic stall and dynamic stall control on helicopter airfoils
Numerical Investigation of Three-Dimensional Static and Dynamic Stall on a Finite Wing
Dynamic Stall Simulations on a Pitching Finite Wing (AIAA 2016-4166)
Detection of Unsteady Boundary Layer Transition Using Three Experimental Methods (AIAA 2016-1072)
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
Dynamic Stall Simulations on a Pitching Finite Wing
Hubschrauberkonfiguration für Hubschrauber mit starrem Horizontalrotor