Titlebook: Computational Fluid Dynamics 2004; Proceedings of the T Clinton Groth,David W. Zingg Conference proceedings 20061st edition Springer-Verlag

coherent

書目名稱Computational Fluid Dynamics 2004影響因子(影響力)




書目名稱Computational Fluid Dynamics 2004影響因子(影響力)學(xué)科排名




書目名稱Computational Fluid Dynamics 2004網(wǎng)絡(luò)公開度




書目名稱Computational Fluid Dynamics 2004網(wǎng)絡(luò)公開度學(xué)科排名




書目名稱Computational Fluid Dynamics 2004被引頻次




書目名稱Computational Fluid Dynamics 2004被引頻次學(xué)科排名




書目名稱Computational Fluid Dynamics 2004年度引用




書目名稱Computational Fluid Dynamics 2004年度引用學(xué)科排名




書目名稱Computational Fluid Dynamics 2004讀者反饋




書目名稱Computational Fluid Dynamics 2004讀者反饋學(xué)科排名

Infuriate

Abundance models in ecology—examplesesilient difficulty. The RANS component also may be improved, with the usual emphasis on separation. Another welcome change would be a numerically efficient system to control laminar regions; a magnificent one would be to predict transition, within the Navier-Stokes solution and even in unstructured grids.

正式演說

bronchodilator

Topics in Detached-Eddy Simulationesilient difficulty. The RANS component also may be improved, with the usual emphasis on separation. Another welcome change would be a numerically efficient system to control laminar regions; a magnificent one would be to predict transition, within the Navier-Stokes solution and even in unstructured grids.

lattice

Computation on Wake/Stator Interaction in a 2D Cascade passage and the full set of passages are presented and compared with the analytical solution, while for the problem of the 4th CAA Workshop, the numerical solution obtained by using two passages is presented.

商議

商議

整頓

Micro Flow Simulation Using Kinetic and Continuum Approacheslts of the Navier-Stokes equations with the slip boundary condition generally agree with those of the kinetic model Boltzmann equation if the Knudsen number is less than 0.1. A kinetic/continuum hybrid method has also been developed. The hybrid method may be a promising tool for analyzing whole flow regimes from free molecule to continuum flows.

HAIL

免費

A Hybrid FE/Spectral Analysis of Turbofan Aeroacousticsproach. The most novel feature of the work is the iterative solution technique using a preconditioner based on an axisymmetric geometry and steady flow field. A numerical example illustrates how few Fourier modes need to be retained, and demonstrates the effectiveness of the preconditioner.