W. Borchers, M. Y. Forestier, S. Kräutle, R. Pasquetti, R.'s Numerical Flow Simulation I: CNRS-DFG Collaborative Research PDF

By W. Borchers, M. Y. Forestier, S. Kräutle, R. Pasquetti, R. Peyret, R. Rautmann, N. Roß (auth.), Prof. Dr. Ernst Heinrich Hirschel (eds.)

ISBN-10: 3540444378

ISBN-13: 9783540444374

ISBN-10: 3642535909

ISBN-13: 9783642535901

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Extra resources for Numerical Flow Simulation I: CNRS-DFG Collaborative Research Programme, Results 1996–1998

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F'. -;-;- --;.. -- - ~ j ~-{)5 8 u ~ :I I!! II. 6 f\ . 8 = 44% spanwise direction. ~ 0 II. 8 = 65% spanwise direction. 06°). 08527. They are within the range of previously computed results listed in [12]. 0°) The flow around a wing-pylon-nacelle configuration (DASA in-house test case) is computed as the second test case. The surface of the configuration consists of 80339 triangles. 0°. The initial grid contains 204725 cells inside the flow domain, of which 86739 cells are intersected by the surface.

If the leaf cell does not contain any other triangle vertex, the current vertex is inserted into this leaf cell. But if the leaf cell already contains another vertex, then the cell is refined until the former vertex and the current vertex are not located inside the same leaf cell any more. For the following calculation of the surface-intersected cells, the sophisticated and efficient neighbour finding algorithm of Samet [17] is applied. 2 Calculation of the Surface-Intersected Cells (Cut-Cells) The body surface splits the intersected Cartesian cells in parts inside and outside the flow field.

11. 1086. This values are slightly smaller, because the methods are not adaptive and therefore especially the shock in the wake is not as well resolved as in this paper. 5 C .!! 5 ! o ! -- I---"' f Il. o (a) Mach contours. 8 (b) Pressure coefficient. 0°) . 0 0 • At this supersonic condition a strong bow shock in front of the airfoil, an oblique shock and a shear layer characterize the Bow, of which the latter two are emanating from the trailing edge. The initial grid has 1309 cells (285 cut-cells).

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Numerical Flow Simulation I: CNRS-DFG Collaborative Research Programme, Results 1996–1998 by W. Borchers, M. Y. Forestier, S. Kräutle, R. Pasquetti, R. Peyret, R. Rautmann, N. Roß (auth.), Prof. Dr. Ernst Heinrich Hirschel (eds.)


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