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EUROSHOCK - Drag Reduction by Passive Shock Control : Results of the Project EUROSHOCK, AER2-CT92-0049 Supported by the European Union, 1993 – 1995
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| 概要 | It has been recognized by the European Union (EU) that the survival of the Aeronautical Industries of Europe in the highly competitive World Aviation Market is strongly dependent on such factors as ti...me-to-market of a new or derivative aircraft and on its manufacturing costs but also on the achievement of a competitive technological advantage by which an increased market share can be gained. Cooperative research is therefore continuously encouraged and co-financed by the European Union in order to strengthen the scientific and technological base of the Aeronautical Industries thus facilitating the future design and manufacture of civil air craft products and providing the technological edge needed for survival. Targets of research within Area 3, Aeronautics, of the Industrial and Materials Technology Programme (1991 - 1993) have been identified to be aircraft efficiency, cost effectiveness and environmental im pact. Concerning aircraft efficiency - relevant to the present research - a reduction in aircraft drag of 10010, a reduction in aircraft fuel consumption of 30010 and a reduction in airframe, en gine and system weight of 20% are envisaged. Meeting these objectives has, of course, also a strong positive impact on the environment. In order to further technology, the philosophy is to avoid spreading the available resources too thinly and rather concentrate on the feasibility demonstration of a limited number of tech nologies of high economic and industrial impact.続きを見る |
| 目次 | A. Synopsis of the Project EUROSHOCK 1 Introduction 2 Basic Experiments and Physical Modeling 3 Extension of Numerical Methods and Preliminary Control Assessment 4 Airfoil Tests with and without Control 5 Assessment of Shock Control - A Summary 6 Overall Conclusion and Future Work 7 References B Individual Contribution 8 Introduction to the Individual Contributions 9 Basic Study of Passive Control Applied to a Two-dimensional Transonic Interaction 10 Passive Control of Shock Wave - Boundary Layer Interaction and Porous Plate Transpiration Flow 11 An Investigation of Passive Control Applied to Swept Shock-Wave/Boundary Layer Interactions 12 Numerical Investigation of the Passive Shock Control on Transonic Airfoils Through an Euler/Boundary-Layer Coupling Technique 13 Introduction of Passive Shock Control in an Interactive Boundary Layer Method 14 Extension, Validation and Application of the DA VII Transonic Airfoil Code with Passive Shock Control 15 Development of Viscous-Inviscid Interaction Codes for Prediction of Shock Boundary-Layer Interaction Control and Buffet over Airfoils 16 Transonic Airfoil Flow Prediction with Shock Boundary Layer Interaction Control by a Time-accurate Navier-Stokes Code 17 Shock Boundary Layer Interaction Control Predictions Using a Viscous-Inviscid Interaction Procedure and a Navier-Stokes Solver 18 Computation of Transonic Flows Applying Shock Boundary Layer Interaction Control 19 Design and Manufacture of the Cryogenic Laminar-type Airfoil DA LVA-1A with Passive Shock Control 20 Qualification by Laser Measurements of the Passive Control on the LVA-1A Airfoil in the T2 Wind Tunnel 21 Experimental Investigation of the Transonic Airfoils DA LVA-1A and VA-2 with Shock Control 22 An Experimental Investigation of Passive Shock/Boundary-Layer Control on an Aerofoil 23 An Experimental Investigation of Passive Shock/Boundary Layer Interaction Control on an Airfoil: Unsteady Measurements.続きを見る |
| 本文を見る | Springer Book Archive - Physics and Astronomy: 1997 |
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| 登録日 | 2026.03.25 |
| 更新日 | 2026.03.25 |