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

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書目名稱EUROSHOCK - Drag Reduction by Passive Shock Control影響因子(影響力)




書目名稱EUROSHOCK - Drag Reduction by Passive Shock Control影響因子(影響力)學(xué)科排名




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書目名稱EUROSHOCK - Drag Reduction by Passive Shock Control被引頻次




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書目名稱EUROSHOCK - Drag Reduction by Passive Shock Control讀者反饋學(xué)科排名

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Basic Study of Passive Control Applied to a Two-dimensional Transonic Interactionly outbalances the gain in wave drag. Also, the rugosity of the holes is an important source of drag (excrescence drag) which contributes to compromise the potential benefit of the passive control technique. The most commonly used turbulence models give poor results, even in the solid wall reference

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Numerical Investigation of the Passive Shock Control on Transonic Airfoils through an Euler/Boundaryn the aerodynamic characteristics of airfoils is concerned, the numerical investigation performed with the present method on the airfoils considered in the project has confirmed the main results of the experiments and of other numerical analyses.

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Transonic Airfoil Flow Prediction with Shock Boundary Layer Interaction Control (SBLIC) by a Time-AcSHOCK..In the unsteady cases a surprisingly good correspondence between calculation and experiment was found with respect to the buffet frequency. However, the start of shock oscillations was predicted at slightly higher Mach numbers / incidences compared to the experiment. In general the 2D Navier-

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0179-9614 ction 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 978-3-322-90713-4978-3-322-90711-0Series ISSN 0179-9614

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https://doi.org/10.1007/b138866ly outbalances the gain in wave drag. Also, the rugosity of the holes is an important source of drag (excrescence drag) which contributes to compromise the potential benefit of the passive control technique. The most commonly used turbulence models give poor results, even in the solid wall reference

微塵

anachronistic

Favorable

Book 1997ess 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

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