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Titlebook: Boundary Integral Methods; Theory and Applicati Luigi Morino,Renzo Piva Conference proceedings 1991 Springer-Verlag Berlin Heidelberg 1991

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11#
發(fā)表于 2025-3-23 11:09:17 | 只看該作者
A Contribution to Lifting Surfaces Aerodynamics Based on Time Domain Aeroacoustics surfaces in linearized compressible flow. The final goal is providing aerodynamic inputs to aeroacoustic codes through the same procedure employed for determining the sound field. Several methods proposed over the last few years have been reviewed; then an aerodynamic formula has been chosen, which
12#
發(fā)表于 2025-3-23 14:28:05 | 只看該作者
Infiltration from Surface Water Bodieslem rests on the determination of the free surface; this is handled by an iteration process along inclined lines, which allow for displacement of the initial guess nodes. A detailed sensitivity analysis was carried out for the number of nodes and the initial guess for the free surface. The results o
13#
發(fā)表于 2025-3-23 18:26:53 | 只看該作者
14#
發(fā)表于 2025-3-24 02:04:11 | 只看該作者
15#
發(fā)表于 2025-3-24 04:35:53 | 只看該作者
Two and Three Dimensional Crack Growth Using the Surface Integral and Finite Element Hybrid Methodor the 3D application, the fatigue growth of a surface crack in a beam under tension is presented. Results obtained using the hybrid method agree very well with experimental data for both opening and shear modes.
16#
發(fā)表于 2025-3-24 09:54:37 | 只看該作者
17#
發(fā)表于 2025-3-24 14:16:44 | 只看該作者
A New Integration Algorithm for Nearly Singular BIE Kernels the point load solution are written as T.(P,Q) and U.(P,Q), respectively. The C. matrix corresponds to the value of the jump in the first integral as the interior displacement evaluation point p(x) is taken to the boundary point P(x).
18#
發(fā)表于 2025-3-24 18:51:36 | 只看該作者
A Contribution to Lifting Surfaces Aerodynamics Based on Time Domain Aeroacoustics was derived by Milliken following an acoustic formulation proposed by Farassat. The method has been improved by adding some correcting terms, as a first step to turn the original lifting surface approach into an actual BEM formulation.
19#
發(fā)表于 2025-3-24 22:52:29 | 只看該作者
Ricardo Guerrero-Lemus,Les E. Shephard vortical flow around the examined configuration. Results of the numerical method concerning aerodynamic loads and flowfield characteristics are discussed and compared to other theoretical models and experimental data.
20#
發(fā)表于 2025-3-25 02:24:18 | 只看該作者
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