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Book Categories |
| A | Synopsis of the Project EUROSHOCK II | 1 |
| 1 | Introduction | 3 |
| 2 | The EUROSHOCK II Project | 9 |
| 3 | Modeling of Active Control Phenomena (Task 1) | 12 |
| 4 | Numerical Simulation of Airfoil and Wing Flow with Control (Task 2) | 38 |
| 5 | Airfoil and Sheared-wing Experiments with and without Control (Task 3) | 72 |
| 6 | Benefits of Control Application to Aircraft Wings/Aircraft (Task 4) | 93 |
| 7 | Assessment of Shock and Boundary Layer Control - A Summary | 114 |
| 8 | Overall Conclusions and Future Work | 116 |
| 9 | References | 121 |
| B | Individual Contributions | 125 |
| 10 | Introduction to the Individual Contributions | 127 |
| 11 | Study of Control Devices Applied to a Transonic Shock Wave/Boundary Layer Interaction | 133 |
| 12 | Hybrid and Active Control of Shock Wave - Turbulent Boundary Layer Interaction and Perforated Plate Transpiration Flow | 153 |
| 13 | Active Control of Swept Shock Wave/Boundary Layer Interactions | 179 |
| 14 | Numerical Investigation of Active Shock Wave and Boundary-Layer Control on Airfoils and Sheared Wings | 205 |
| 15 | Euler/Boundary Layer Coupling to Predict Steady and Unsteady Transonic Flows Past an Airfoil with and without Shock Control | 237 |
| 16 | 2D Numerical Investigations of Shock and Boundary Layer Control Techniques | 255 |
| 17 | Prediction of Transonic Airfoil/Wing Flow and Buffet with Control Using a Time-accurate Viscous-Inviscid Interaction Approach | 285 |
| 18 | Steady and Unsteady Numerical NS-Calculations for the DRA-2303 Airfoil with and without Bump | 315 |
| 19 | An Investigation of Active, Suction, Shock and Boundary-Layer Control Techniques | 331 |
| 20 | Experimental Investigation of the Transonic Airfoils ADIF and DA LVA-1A and the ADIF Sheared Wing with and without Control | 359 |
| 21 | Assessment of Shock and Boundary Layer Control Concepts for Hybrid Laminar Flow Wing Design | 383 |
| 22 | Assessment of Bump Control and its Application to a Long-range Turbulent-wing Aircraft | 415 |
| 23 | Drag Reduction and Buffet Damping by a Contour Bump Control Device and Regional-jet Application | 417 |
| 24 | Application of Shock and Boundary Layer Control to a Business-jet Aircraft | 433 |
| Price | Condition | Delivery | Seller | Action |
| $299.00 | Digital |
| WonderClub |
Brian Gonsalves
reviewed Drag Reduction by Shock and Boundary Layer Control on September 28, 2013
Drag Reduction by Shock and Boundary Layer Control
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