Titlebook: High Performance Computing in Science and Engineering, Garching/Munich 2009; Transactions of the Siegfried Wagner,Matthias Steinmetz,Marku

Arable

Assessment of CFD Predictive Capability for Aeronautical Applicationsady Reynolds Averaged Navier Stokes and Scale-Adaptive Simulations are carried out to predict the flow physics of such complex geometry arrangements. The simulation results show a satisfactory agreement with a wide range of experimental data.

可用

insecticide

薄荷醇

Numerical Experiments for Quantification of Small-Scale Effects in Particle-Laden Turbulent Flowre kinetic energy of the unresolved scales is lower than average. This effect was so far neglected in most LES models for particle-laden flow. Furthermore, the results show that locations for particle clustering and mechanisms leading to clustering are dominated by large-scale dynamics, a promising result for LES.

天然热喷泉

Vorticity Statistics in Fully Developed Turbulencect numerical simulations. A parallel pseudospectral code is used to to obtain well-resolved numerical simulations of homogeneous isotropic turbulence. The results yield a consistent description of the vorticity statistics and provide insights into the structure and dynamics of fully developed turbulence.

啪心儿跳动

Incorruptible

images represents a challenging problem that requires a huge computational effort. This work proposes the use of metaheuristic algorithms, combined with segmentation techniques and thermal images, to detect faults and contribute to the preventive maintenance of electronic systems.

forestry

发怨言

Performance Limitations for Sparse Matrix-Vector Multiplications on Current Multi-Core Environmentspectively: compressed row and jagged diagonal storage. Starting from a series of microbenchmarks to single out performance limitations, we apply the gained insight to optimize sparse MVM implementations, reviewing serial and OpenMP-parallel performance on state-of-the-art multi-core systems.

吹牛者

Capability of FDEM for Journal Bearings with Microstructured Surface with different microstructure for Reynolds number .=24,500, and we also give a global error estimate for each of the cases. This shows the quality of the numerical solution and is a unique feature of FDEM. Furthermore, we demonstrate the scalability of the code.