Titlebook: Drag Reduction by Shock and Boundary Layer Control; Results of the Proje Egon Stanewsky,Jean Délery,Paolo Matteis Conference proceedings 20

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1612-2909 n Market is strongly dependent on such factors as time-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. Recognizing this, cooperative research is continuousl

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Conference proceedings 2002-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. Recognizing this, cooperative research is continuously encouraged and co-financed by the European Union in ord

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Steady and Unsteady Numerical NS-Calculations for the DRA 2303 Airfoil with and without Bumpe calculations have shown that agreement was achieved in most cases. As far as steady drag calculations are concerned, at least the right tendencies have been predicted, although the absolute values differed from the experimental data.

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Euler/Boundary Layer Coupling to Predict Steady and Unsteady Transonic Flows Past an Airfoil with ann of buffet onset is consistent with other methods, but quantitative differences have been found. Results clearly indicate that control devices can be helpful in reducing drag and in delaying buffet onset to higher lift coefficients or Mach numbers.