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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Experimental Investigation of the Transonic Airfoils ADIF and DA LVA-1A and the ADIF Sheared Wing win terms of cruise drag, hence speed and/or fuel consumption, and with respect to the drag-rise and buffet boundaries. An extensive wind tunnel program on airfoils and an infinitely-swept sheared wing was, therefore, carried out investigating the effect of shock and boundary layer control on the impr

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Assessment of Bump Control and its Application to a Long-range Turbulent-wing Aircrafttrol to an A340-type aircraft wing of existing turbulent design and to determine benefits and penalties of control implementation on the operational aircraft. The control mechanism considered was foremost the contour bump. (Originally, also a new turbulent wing design with integrated bump should hav

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Drag Reduction and Buffet Damping by a Contour Bump Control Device and Regional-jet Application drag in transonic flow and to allow damping of aerodynamic buffet. Evaluations on 2D airfoils have been performed using the ALN Navier-Stokes code. Indications have been obtained that a local, well designed, upper surface deformation (bump) can sensibly reduce airfoil drag in transonic flow in a la

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Drag Reduction by Shock and Boundary Layer Control978-3-540-45856-2Series ISSN 1612-2909 Series E-ISSN 1860-0824

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Charles C. J. Carpenter,Richard B. Hornickmining the design and off-design performance of transonic transport aircraft in the case of a turbulent wing but more so for laminar wings where moderate to strong shock waves may already be present at cruise conditions in order to take full advantage of the potential of laminarization. Based on the

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