Soji Yamakawa and Kenji Shimada GOAL

Slides:



Advertisements
Similar presentations
Steady-state heat conduction on triangulated planar domain May, 2002
Advertisements

CandeCAD Overview UTILITY Step 1: MESH DESIGN Step 2: ASSIGN INTELLIGENCE Step 3: CONDUCT ANALYSIS Step 4: IMPORT RESULTS.
Finite element method Among the up-to-date methods of stress state analysis, the finite element method (abbreviated as FEM below, or often as FEA for analyses.
By: Rachel Sorna and William weinlandt
© Fluent Inc. 4/16/ Introductory GAMBIT Notes GAMBIT v2.0 Jan 2002 Fluent User Services Center Edge and Face Meshing.
1 Lecture 7 - Meshing Applied Computational Fluid Dynamics Instructor: André Bakker © André Bakker ( ) © Fluent Inc. (2002)
Workshop 15 Hybrid meshing of a simple HVAC assembly
The Effect of T-Stiffener Web and Flange Tilt on Frame Stress Evaluated using Finite Element Analysis by Dean Pasquerella MASTER OF ENGINEERING Major Subject:
VIRTUAL ARTHROSCOPIC KNEE SURGERY TRANING SYSTEM Yang Xiaosong The Chinese University of Hong Kong Tsinghua University.
Coupling Continuum Model and Smoothed Particle Hydrodynamics Methods for Reactive Transport Yilin Fang, Timothy D Scheibe and Alexandre M Tartakovsky Pacific.
Evan Greer, Mentor: Dr. Marcelo Kobayashi, HARP REU Program August 2, 2012 Contact: globalwindgroup.com.
Review: CFD Step by Step
Chapter 1 Introduction to CFD
Copyright 2001, J.E. Akin. All rights reserved. CAD and Finite Element Analysis Most ME CAD applications require a FEA in one or more areas: –Stress Analysis.
Coupled Fluid-Structural Solver CFD incompressible flow solver has been coupled with a FEA code to analyze dynamic fluid-structure coupling phenomena CFD.
Nut, washer and locking device removed from model.
Thermo-fluid Analysis of Helium cooling solutions for the HCCB TBM Presented By: Manmeet Narula Alice Ying, Manmeet Narula, Ryan Hunt and M. Abdou ITER.
Homework 3: Use the Fixed Grid --Volume of Fluid Method with Structured Cartesian CVFEM mesh To track Filling Front h=1 h = 0 2 r = 1 3 Hand in 1. Code.
ECIV 720 A Advanced Structural Mechanics and Analysis Solid Modeling.
Steady Aeroelastic Computations to Predict the Flying Shape of Sails Sriram Antony Jameson Dept. of Aeronautics and Astronautics Stanford University First.
Physically-Based Simulation of Objects Represented by Surface Meshes Matthias Muller, Matthias Teschner, Markus Gross CGI 2004.
Introduction to Finite Element Analysis for Structure Design Dr. A. Sherif El-Gizawy.
Scientific Visualization Data and Geometry Processing for Scientific Visualization CS 5630 / 6630 August 28, 2007.
© T Madas.
COMPUTER-AIDED DESIGN The functionality of SolidWorks Simulation depends on which software Simulation product is used. The functionality of different producs.
Applications of Adjoint Methods for Aerodynamic Shape Optimization Arron Melvin Adviser: Luigi Martinelli Princeton University FAA/NASA Joint University.
© 2011 Autodesk Freely licensed for use by educational institutions. Reuse and changes require a note indicating that content has been modified from the.
1 Finite-Volume Formulation. 2 Review of the Integral Equation The integral equation for the conservation statement is: Equation applies for a control.
By Chris Klobedanz MANE-4240 Final Project. Purpose Evaluate the Natural Frequencies of a Steel Cantilever Beam System Compare the Results of Beams with.
Wing Embedded Engines For Large Blended Wing Body Aircraft
March 12, 2008 A Parallel Algorithm for Optimization-Based Smoothing of Unstructured 3-D Meshes by Vincent C. Betro.
Grid Generation.
Introduction to CFD Analysis
Chapter 3 Meshing Methods for 3D Geometries
Training Manual Aug Element Technology Overview: In this chapter, we will present a brief overview to the following topics: A.
ANSYS, Inc. Proprietary © 2004 ANSYS, Inc. Chapter 6 ANSYS CFX 9.0.
Problem Definition: Solution of PDE’s in Geosciences  Finite elements and finite volume require: u 3D geometrical model u Geological attributes and u.
Adaptive Meshing Control to Improve Petascale Compass Simulations Xiao-Juan Luo and Mark S Shephard Scientific Computation Research Center (SCOREC) Interoperable.
Course 8 Contours. Def: edge list ---- ordered set of edge point or fragments. Def: contour ---- an edge list or expression that is used to represent.
Results Summary and Images Data Analysis The control school bus model had a higher C D than theoretically expected; compared to a theoretical
Version 1.0 3/23/2007 © 2007 ANSYS, Inc. All rights reserved. Inventory # W6-1 BladeModeler 11.0 ANSYS, Inc. Proprietary BladeModeler 11.0 Practical.
CAD and Finite Element Analysis Most ME CAD applications require a FEA in one or more areas: –Stress Analysis –Thermal Analysis –Structural Dynamics –Computational.
COMSOL Analysis: End Loaded Cantilever Beams of Various Cross Sections Gregory Hew.
Meta-controlled Boltzmann Machine toward Accelerating the Computation Tran Duc Minh (*), Junzo Watada (**) (*) Institute Of Information Technology-Viet.
Version 1.0 3/23/2007 © 2007 ANSYS, Inc. All rights reserved. Inventory # W3-1 BladeModeler 11.0 ANSYS, Inc. Proprietary ANSYS BladeModeler 11.0.
WS4.3-1 ANSYS, Inc. Proprietary © 2009 ANSYS, Inc. All rights reserved. July 2009 Inventory # Chapter 4 Volume Meshing – Workshop 3 Femur BF Cartesian.
Computational Fluid Dynamics Lecture II Numerical Methods and Criteria for CFD Dr. Ugur GUVEN Professor of Aerospace Engineering.
Chapter 5.1 Mesh Preparation and Output to Solver
Chapter 3 Shell Meshing – Workshop 2 Wingbody – F6 Model
Objective: Be able to work out the volume of a prism.
Chapter 5 Prism Meshing – Workshop 1 Waterjacket Section
Edge and Face Meshing.
Free vs. Forced Convection
Lecture 7 - Meshing Applied Computational Fluid Dynamics
FEM 1D Programming Term Project
CAD and Finite Element Analysis
Accurate viscoelastic large deformation analysis using F-bar aided edge-based smoothed finite element method for 4-node tetrahedral meshes (F-barES-FEM-T4)
© Fluent Inc. 8/24/ Introductory FLUENT Notes FLUENT v6.0 Jan 2002 Fluent User Services Center Introduction to CFD Analysis.
Convergence in Computational Science
Fluid Flow Regularization of Navier-Stokes Equations
The application of an atmospheric boundary layer to evaluate truck aerodynamics in CFD “A solution for a real-world engineering problem” Ir. Niek van.
ECIV 720 A Advanced Structural Mechanics and Analysis
Meshing Strategy.
Volume Meshing.
Simplification and Improvement of Tetrahedral Models for Simulation
Thermal behavior of the LHCb PS VFE Board
Finite elements Pisud Witayasuwan.
Linear strain triangular Tieme Willems
Mesh Morph 2.0 Tutorial 7/29/2019.
Auxiliary view method.
Presentation transcript:

Converting a Tetrahedral Mesh to a Prism-Tetrahedral Hybrid Mesh for FEM Accuracy and Efficiency Soji Yamakawa and Kenji Shimada GOAL Converting a tetrahedral mesh into a prism-tetrahedral mixed mesh. A prism-tetrahedral hybrid mesh yields a more accurate FEM solution with less computational time than a tetrahedral mesh. APPROACH The proposed method progressively inserts layers of prism elements in sweepable sub-volumes starting from a given cross section. Prism-Layer Insertion Input Tetrahedral Mesh 5,994 nodes 25,013 elements After 4 Layers are Inserted Final Prism+Tet Mesh 5,858 nodes 18,319 tet elements 1,960 prism elements 20,279 elements in total No more prism layer can be inserted without violating a prescribed quality threshold Frontal Plane Cutting Plane (Initial Frontal Plane) Cross Section Undo-able Data Structure Apply sequence of edge-collapse, local transformation, and smoothing operations to remove nodes that obstructs a new prism layer A new prism layer is inserted if: (1) All nodes obstructing the new layer insertion are removed, and (2) No element violates the quality threshold. Undo-able data structure overcomes the order-dependency problem of the mesh-modifying operations. If an element violates the quality threshold, the modifications must be retracted, and the proposed method tries a different sequence of mesh-modifying operations Effect of the Prism-Layer Insertion Error Tetrahedral Mesh Prism-Tet Hybrid Mesh 0.00000 0.00400 0.00800 0.01200 20000 40000 60000 80000 100000 # of elements Convergence of the Error Between Two Outlet Fluxes CFD Analysis of an Air-Conditioner Duct CFD Solution converges (reaches as accurate as it can) faster with a prism-tet hybrid mesh than a tetrahedral mesh. Structural Analysis of a Leg-Bone