Titlebook: EUROSHOCK - Drag Reduction by Passive Shock Control; Results of the Proje Egon Stanewsky,Jean Délery,Wolfgang Geißler Book 1997 Springer Fa

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Extension of Numerical Methods and Preliminary Control Assessment (Task 2) validated by the airfoil experiments of Task 3 and used for a preliminary assessment of the merits of passive shock control. A total of seven contributors have participated in the numerical studies, namely, . and the Universities of . and ..

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Introductiono study, numerically and experimentally, the effect of passive shock boundary layer interaction control (SBLIC) by ventilation on the design and off-design performance of primarily laminar-type airfoils and wings. The considerations leading to this research are outlined in what follows.

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Overall Conclusion and Future Workement in the buffet boundary can be achieved. Also other configurations, such as engine inlets, where passive control may be of merit, have been identified The investigations have furthermore shed new light on the complex subject of shock wave boundary layer interaction and have highlighted new acti

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