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Drag Reduction by Shock and Boundary Layer Control [2002]
- 1
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Synopsis of the Project EUROSHOCK II
- 127
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Introduction to the Individual Contributions
- 133
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Study of Control Devices Applied to a Transonic Shock Wave/Boundary Layer Interaction
- 153
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Hybrid and Active Control of Shock Wave — Turbulent Boundary Layer Interaction and Perforated Plate Transpiration Flow
- 179
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Active Control of Swept Shock Wave / Boundary Layer Interactions
- 205
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Numerical Investigation of Active Shock Wave and Boundary-Layer Control on Airfoils and Sheared Wings
- 237
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Euler/Boundary Layer Coupling to Predict Steady and Unsteady Transonic Flows Past an Airfoil with and without Shock Control
- 255
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2D Numerical Investigations of Shock and Boundary Layer Control Techniques
- 285
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Prediction of Transonic Airfoil/Wing Flow and Buffet with Control Using a Time-accurate Viscous-Inviscid Interaction Approach
- 315
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Steady and Unsteady Numerical NS-Calculations for the DRA 2303 Airfoil with and without Bump
- 331
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An Investigation of Active, Suction, Shock and Boundary Layer Control Techniques
- 359
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Experimental Investigation of the Transonic Airfoils ADIF and DA LVA-1A and the ADIF Sheared Wing with and without Control
- 383
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Assessment of Shock and Boundary Layer Control Concepts for Hybrid Laminar Flow Wing Design
- 415
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Assessment of Bump Control and its Application to a Long-range Turbulent-wing Aircraft
- 417
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Drag Reduction and Buffet Damping by a Contour Bump Control Device and Regional-jet Application
- 433
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Application of Shock and Boundary Layer Control to a Business-jet Aircraft