Orthogonal H-type and C-type grid generation for 2-d twin deck bridge Xiaobing Liu, Chaoqun Liu, Zhengqing Chen Mathematic Department, University of Texas.

Slides:



Advertisements
Similar presentations
MASS TRANSFER TO SPHERE AND HEMISPHERE ELCTRODES BY IMPINGING JET
Advertisements

21 November 2007 Phys. Sc. & Engin. Grad School, Cardiff VISCOELASTIC FLUIDS: A BRIEF DESCRIPTION AND SOME MAIN FEATURES EXTRUDATE SWELL EXTRUDATE SWELL.
Active Contours, Level Sets, and Image Segmentation
The analysis of the two dimensional subsonic flow over a NACA 0012 airfoil using OpenFoam is presented. 1) Create the geometry and the flap Sequence of.
P. Venkataraman Mechanical Engineering P. Venkataraman Rochester Institute of Technology DETC2013 – 12269: Continuous Solution for Boundary Value Problems.
P. Venkataraman Mechanical Engineering P. Venkataraman Rochester Institute of Technology DETC2014 – 35148: Continuous Solution for Boundary Value Problems.
Airbreathing Hypersonics Laboratory China Aerodynamics Research and Development Center Osculating Inward turning Cone Waverider/Inlet (OICWI) Design Analysis.
Interactive System for Pulverized Coal Combustion Visualization with Fluid Simulator Marek Gayer, Pavel Slavík and František Hrdlička Department of Computer.
MAE 3241: AERODYNAMICS AND FLIGHT MECHANICS
2L 2aL s h T Introduction Zach Frye, University of Wisconsin-Eau Claire Faculty Advisors: Mohamed Elgindi, and John Drost, Department of Mathematics Funded.
PREPARED BY: JANAK GAJJAR SD1909.  Introduction  Wind calculation  Pressure distribution on Antenna  Conclusion  References.
Computer Simulations of Wind Tunnel Experiments
A Bezier Based Approach to Unstructured Moving Meshes ALADDIN and Sangria Gary Miller David Cardoze Todd Phillips Noel Walkington Mark Olah Miklos Bergou.
PART 7 Ordinary Differential Equations ODEs
Finite Element Method Introduction General Principle
Multi-Scale Finite-Volume (MSFV) method for elliptic problems Subsurface flow simulation Mark van Kraaij, CASA Seminar Wednesday 13 April 2005.
Theoretical & Industrial Design of Aerofoils P M V Subbarao Professor Mechanical Engineering Department An Objective Invention ……
Potential Flow Theory for Development of A Turbine Blade
Types of Governing equations
Application of Digital Signal Processing in Computed tomography (CT)
Copyright © 2006 The McGraw-Hill Companies, Inc. Permission required for reproduction or display. by Lale Yurttas, Texas A&M University Part 81 Partial.
1 Finite-Volume Formulation. 2 Review of the Integral Equation The integral equation for the conservation statement is: Equation applies for a control.
Lecture 24 Introduction to state variable modeling Overall idea Example Simulating system response using MATLAB Related educational modules: –Section 2.6.1,
1 CFD Analysis Process. 2 1.Formulate the Flow Problem 2.Model the Geometry 3.Model the Flow (Computational) Domain 4.Generate the Grid 5.Specify the.
Introduction to virtual engineering László Horváth Budapest Tech John von Neumann Faculty of Informatics Institute of Intelligent Engineering.
Ming-Yi Liu Yu-Jie Li Reliability Analysis of High-Rise Buildings under Wind Loads Department of Civil Engineering, Chung Yuan Christian University, Taiwan.
한국강구조학회 2001 년도 학술발표대회 Three Dimensional Finite Element Analysis of Structures under Wind Loads *Byoung-Wan Kim 1), Woon-Hak Kim 2) and In-Won Lee 3) 1)
Teaching Partial Differential Equations Using Mathematica Katarina Jegdic Assistant Professor Computer and Mathematical Sciences Department University.
Partial Differential Equations Finite Difference Approximation.
LESSON LD04 Aerodynamics
Brookhaven Science Associates U.S. Department of Energy MUTAC Review January 14-15, 2003, FNAL Target Simulations Roman Samulyak Center for Data Intensive.
Supercomputing Center CFD Grid Research in N*Grid Project KISTI Supercomputing Center Chun-ho Sung.
A conservative FE-discretisation of the Navier-Stokes equation JASS 2005, St. Petersburg Thomas Satzger.
Incompressible Flow over Airfoils
Numerical Investigation into Potential Flow Around High-speed Hydrofoil Assisted Craft ZHONGYU YANG supervised by Prof G.E HEARN and.
Robustness of complex networks with the local protection strategy against cascading failures Jianwei Wang Adviser: Frank,Yeong-Sung Lin Present by Wayne.
Copyright © The McGraw-Hill Companies, Inc. Permission required for reproduction or display. 1 Part 8 - Chapter 29.
Silesian University of Technology in Gliwice Inverse approach for identification of the shrinkage gap thermal resistance in continuous casting of metals.
HEAT TRANSFER FINITE ELEMENT FORMULATION
Challenges in Wind Turbine Flows
COMPUTATIONAL FLUID DYNAMICS (AE 2402) Presented by IRISH ANGELIN S AP/AERO.
Thin Aerofoil Theory for Development of A Turbine Blade
1 Zonal Boundary Conditions. 2 Some Basics The flow domain is divided into zones and grids are generated within each zone. The flow equations are solved.
Solving Partial Differential Equation Numerically Pertemuan 13 Matakuliah: S0262-Analisis Numerik Tahun: 2010.
M. Khalili1, M. Larsson2, B. Müller1
MSC Software India User Conference 2012 September 13-14, 2012 Bangalore, India CFD Based Frequency Domain Flutter Analysis using MSC Nastran Ashit Kumar.
PRESENTATION OUTLINE Experiment Objective Introduction Data Conclusion Recommendations.
A Simulation Framework for Testing Flow Control Strategies Marek Gayer, Milan Milovanovic and Ole Morten Aamo Faculty of Information Technology, Mathematics.
Computational Fluid Dynamics Lecture II Numerical Methods and Criteria for CFD Dr. Ugur GUVEN Professor of Aerospace Engineering.
1 Line Integrals In this section we are now going to introduce a new kind of integral. However, before we do that it is important to note that you will.
LESSON LD04 Aerodynamics
MAE 3241: AERODYNAMICS AND FLIGHT MECHANICS
Part 8 - Chapter 29.
Fluid Structure Interactions Research Group
P M V Subbarao Professor Mechanical Engineering Department
Prepared BY: Helwan University Faculty Of Engineering
Boundary Element Analysis of Systems Using Interval Methods
Xiaomin Pang, Yanyan Chen, Xiaotao Wang, Wei Dai, Ercang Luo
Introduction to Partial Differential Equations
LESSON LD04 Aerodynamics
AE/ME 339 Computational Fluid Dynamics (CFD) K. M. Isaac
Brief introduction to Partial Differential Equations (PDEs)
College Algebra Chapter 5 Systems of Equations and Inequalities
Partial Differential Equations
Step change in the boundary condition of conduction problems
Relaxation Technique CFD
LESSON LD04 Aerodynamics
AE/ME 339 Computational Fluid Dynamics (CFD) K. M. Isaac
AE/ME 339 Computational Fluid Dynamics (CFD) K. M. Isaac
Presentation transcript:

Orthogonal H-type and C-type grid generation for 2-d twin deck bridge Xiaobing Liu, Chaoqun Liu, Zhengqing Chen Mathematic Department, University of Texas at Arlington , USA Wind engineering research center , Hunan University, China 7TH AIMS CONFERENCE

Main Content  Background  Introduction to grid generation method  Result  Conclusion

Background In recent years, as traffic amount increasing, decks of bridges are becoming wider and wider. A new kind of bridge, twin deck bridges were built all over the world because of good visual effect and traffic condition. Fred Hartman bridge (Texas, USA) Tacoma bridge (Washington, USA)

Qing dao Bay Bridge, Shan dong Province, China Ping sheng Bridge, Guang dong Province, China Since two decks of twin deck bridge are very closed to each other, in strong wind, the flow around decks will make wind load, vortex shedding and flutter stability of decks different from those of common single deck. We call this aerodynamic interference effect of twin deck bridge.

The aerodynamic interference effect of twin deck bridge is influenced by many factors, such as geometric shape of deck cross section 、 distance of two decks 、 wind attack angle and so on. It is more feasible to choose numerical simulation It will cost lots of money and energy to do wind tunnel test

Basic idea of numerical simulation : Discretisise the governing equations of fluid ( partial differential equations) into basic linear equations on numerical grid. Solve the linear equations to get general variables of fluid, such as velocity, pressure and etc around bridge decks. Numerical grid is the basis of numerical computing. The quality of numerical grid, such as smoothness and orthogonality plays a crucial role in affecting numerical computing result. In the following sections, orthogonal H type and C type grids were generated for 2-d Qing dao Bay bridge and 2-d simplified twin deck bridge model using numerical method.

Introduction to grid generation method The basic idea of grid generation method we used was mentioned firstly by S.P.Spekreijse in his paper “ Elliptic Grid Generation Based on Laplace Equations and Algebraic Transformation”. Here we will give a introduction to this method through following simple geometry.

algebraic transformation elliptic transformation computational domain parameter domain physical domain

The grid generation mainly consists of following three steps. The first step aims to generate a simple but not smooth algebraic grid in physical domain based on transfinite interpolation. According to the grids on the boundary of the physical domain and grids in the computational domain, grid distribution in the interior of physical domain can be obtained based on following equations.

physical domain

The second step is to make the algebraic grid in physical domain to be smooth and stretched. elliptic transformation from parameter domain to physical domain where,,, algebraic transformation from computational domain to parameter domain where and are normalized arc-lengths along four boundary edges.

Compositing these two transformations, we get where,, By solving above equations using finite difference method, we can get smooth and stretched grid in physical domain.

parameter domain physical domain

The third step is to make grid in physical domain to be orthogonal on boundaries. In order to get orthogonal grid on boundary E3, we can first solve two Laplace equations and with following boundary condition to get new s and t. Where n is the outward normal direction at boundary E3 and E4 Where n is the outward normal direction at boundary E1 and E2

After that, we re-compute and based on boundary function of above s and t using following Hermite interpolation. where At last we go back to the second step to get new x and y.

parameter domain physical domain

result complete griddetail of grid on deck surface H-type grid for Qing Dao Bay bridge

complete grid detail of grid on deck surface C-type grid for Qing Dao Bay bridge

H-type grid for twin deck bridge model complete grid detail of grid on deck surface

C-type grid for twin deck bridge model complete grid detail of grid on deck surface

Conclusion There exists aerodynamic interference effect between two decks of twin deck bridge. Both C-type and H-type grids have been generated for a 2-d twin deck bridge and 2-d simplified twin deck bridge model using numerical method. The grids are smooth and orthogonal on deck surface and computational boundary. This provides an effective guarantee for studying on aerodynamic interference effect of twin deck bridge using numerical method.

Thank you !