DIFFERENTIAL DISTANCE FUNCTION COMPUTATIONS FOR MESH GENERATION
DIFFERENTIAL DISTANCE FUNCTION COMPUTATIONS FOR MESH GENERATION
批准号:
EP/E057233/1
负责人:
Paul G. Tucker
金额:
$34.18万
依托单位:
依托单位国家:
英国
项目类别:
Research Grant
财政年份:
2007
资助国家:
英国
项目状态:
已结题
起止时间:
2007 至 --
中文摘要
点击翻译按钮获取中文摘要
英文摘要
Essentially, distance functions (raw and modified nearest surface distances) are needed for RANS (Reynolds Averaged Navier-Stokes) turbulence modelling, general computational interface tracking for multiphase and free surface flows, electrostatic Coulomb force modelling and also flame front and explosion modelling along with ray tracing for optics and acoustics. They can also be used to capture Knudsen layer effects in microscale flows and for the implementation sponges and various other numerical wave reflection damping strategies and stabilising measures for LES (Large Eddy Simulation). Furthermore they can be used to implement hybrid LES-RANS strategies. Distance functions, can under certain circumstances be evaluated using expensive search operations. Alternatively, differential equations can be solved. Here, it is proposed to explore the solution of differential distance function equations on unstructured (where a wide range of cell shapes can be tessellated in a flexible fashion) moving and overset meshes to yield the above noted capabilities which are highly desirable for general purpose CFD codes. Flow solutions using such grids are increasingly common. However, robust mesh generation still presents a significant challenge. This is especially so if use is made of hexahedral cells and the higher numerical fidelity that they provide. Hence, here it is proposed to also explore the use of novel differential distance function related equation based approaches for: hybrid grid generation (hexahedral boundary layer cells linked to tetrahedral cells outside the boundary layer); pure hexahedral grid generation and overset grid computational interface location. The differential equations explored will include the hyperbolic Eikonal, Hamilton-Jacobi and elliptic Poisson. Especial attention will be paid to the economical and accurate solution of these equations on moving, unstructured over-set grids with mixed element topologies using finite element, finite volume & boundary element methods.
期刊论文(10)
专著(0)
科研奖励(0)
会议论文
登录
查看更多内容
DOI:
--
发表时间:
2009
期刊:
影响因子:
--
作者:
[H Xia]
通讯作者:
H Xia
DOI:
10.1016/j.paerosci.2010.03.001
发表时间:
2010-10
期刊:
Progress in Aerospace Sciences
影响因子:
9.6
作者:
[H. Xia;P. Tucker;W. Dawes]
通讯作者:
H. Xia;P. Tucker;W. Dawes
Differential equations for generating multiblock mesh partitions
用于生成多块网格分区的微分方程
DOI:
--
发表时间:
期刊:
影响因子:
--
作者:
[Paul G. Tucker (Co-Author)]
通讯作者:
Paul G. Tucker (Co-Author)
Hybrid Hamilton-Jacobi-Poisson wall distance function model
混合 Hamilton-Jacobi-Poisson 壁距离函数模型
DOI:
10.1016/j.compfluid.2010.12.021
发表时间:
2011
期刊:
Computers & Fluids
影响因子:
2.8
作者:
[Tucker P]
通讯作者:
Tucker P
Numerical Study of Chevron Jet Noise Using Parallel Flow Solver
使用并行流求解器对 Chevron 喷射噪声进行数值研究
DOI:
10.1016/j.proeng.2013.07.090
发表时间:
2013
期刊:
Procedia Engineering
影响因子:
--
作者:
[Xia H]
通讯作者:
Xia H
共 7 条
AEROENGINE AEROACOUSTIC INTERACTIONS
-
批准号:EP/I010440/1
-
项目类别:Research Grant
-
资助金额:$56.27万
-
财政年份:2011
-
负责人:Paul G. Tucker
-
依托单位:
AERODYNAMICS & AEROACOUSTICS OF COMPLEX GEOMETRY HOT JETS
-
批准号:EP/I017771/1
-
项目类别:Research Grant
-
资助金额:$55.6万
-
财政年份:2011
-
负责人:Paul G. Tucker
-
依托单位:
SAMULET Project 1 - High Efficiency Turbomachinery
-
批准号:EP/H001395/1
-
项目类别:Research Grant
-
资助金额:$185.28万
-
财政年份:2009
-
负责人:Paul G. Tucker
-
依托单位:
CAMBRIDGE UGTP WHOLE ENGINE COMPUTATIONAL AEROACOUSTICS CONSORTIUM
-
批准号:EP/G027633/1
-
项目类别:Research Grant
-
资助金额:$11.5万
-
财政年份:2009
-
负责人:Paul G. Tucker
-
依托单位:
海外基金