Modern Transition Prediction Techniques Based on Adjoint Methods
The Importance of Aerodynamics in the Development of Commercially Successful Transport Aircraft
Current Status and Prospects for Turbulent Flow Control
Drag Reduction in Airfoils Using Control Devices in the Shock Wave-Boundary Layer Interaction Region
Next Steps Envisaged to Improve Wing Performance of Commercial Aircraft
Lessons Learned from Dassault's Falcon 900 HLF Demonstrator
Control of the Coherent Vortical Structures of a Boundery Layer
European Research to Reduce Drag for Supersonic Transport Aircraft
Aspects of Shock Control and Adaptive Wing Technology
Retrofit Studies based on Airbus A310 for HLFC Application on Aircrafts
DNS Study of Suction Through Arrays of Holes in a 3-D Boundary-Layer Flow
Industrial Perspectives of Drag Reduction Technologies