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Drag Reduction by Shock and Boundary Layer Control [2002]

1
Synopsis of the Project EUROSHOCK II
127
Introduction to the Individual Contributions
133
Study of Control Devices Applied to a Transonic Shock Wave/Boundary Layer Interaction
153
Hybrid and Active Control of Shock Wave — Turbulent Boundary Layer Interaction and Perforated Plate Transpiration Flow
179
Active Control of Swept Shock Wave / Boundary Layer Interactions
205
Numerical Investigation of Active Shock Wave and Boundary-Layer Control on Airfoils and Sheared Wings
237
Euler/Boundary Layer Coupling to Predict Steady and Unsteady Transonic Flows Past an Airfoil with and without Shock Control
255
2D Numerical Investigations of Shock and Boundary Layer Control Techniques
285
Prediction of Transonic Airfoil/Wing Flow and Buffet with Control Using a Time-accurate Viscous-Inviscid Interaction Approach
315
Steady and Unsteady Numerical NS-Calculations for the DRA 2303 Airfoil with and without Bump
331
An Investigation of Active, Suction, Shock and Boundary Layer Control Techniques
359
Experimental Investigation of the Transonic Airfoils ADIF and DA LVA-1A and the ADIF Sheared Wing with and without Control
383
Assessment of Shock and Boundary Layer Control Concepts for Hybrid Laminar Flow Wing Design
415
Assessment of Bump Control and its Application to a Long-range Turbulent-wing Aircraft
417
Drag Reduction and Buffet Damping by a Contour Bump Control Device and Regional-jet Application
433
Application of Shock and Boundary Layer Control to a Business-jet Aircraft
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