Titlebook: Control of Flow Instabilities and Unsteady Flows; G. E. A. Meier,G. H. Schnerr Book 1996 Springer-Verlag Wien 1996 flow.fluid mechanics.me

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Diskurstheorie als Forschungsperspektivey supersonic compressor flow. Alternatively we show the effectiveness of ventilation by very thin slits instead of a cavity covered by a porous blade..Finally we apply the method of ventilation to unsteady internal transonic flow. Experiments and numerical results of the Euler equations for inviscid

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Control of Laminar-Turbulent Transition for Skin Friction Drag Reduction,and illustrated by experimental results obtained in wind tunnel or in free flight conditions. Wave cancellation techniques are also presented. An important part of the paper is devoted to the use of the linear stability theory as a practical tool for transition prediction.

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Diskurstheorie als Forschungsperspektive the abilities of applied methods. Finally, the material presented here, describes some of the modifications being introduced to standard passive control in order to improve the effectiveness of ventilation.

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Passive Control of Shock/Boundary Layer Interaction, the abilities of applied methods. Finally, the material presented here, describes some of the modifications being introduced to standard passive control in order to improve the effectiveness of ventilation.

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Diskurstheorie als Forschungsperspektive experimental and numerical results concerning the following techniques: wall suction, injection, active and selective control of turbulent boundary layers, passive control of turbulent boundary layers using LEBUs and Riblets. Some turbulent separation flow control will be briefly evoked.

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Developments in Stability Theory,isk, and the stability of a range of wake flows. All these situations apply very much to parallel flows, however, and in order to handle non-parallel flows one must find ways of connecting the local, quasi-parallel properties of the flow to the global dynamics.

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Control of Turbulent Flows for Skin Friction Drag Reduction, experimental and numerical results concerning the following techniques: wall suction, injection, active and selective control of turbulent boundary layers, passive control of turbulent boundary layers using LEBUs and Riblets. Some turbulent separation flow control will be briefly evoked.