ANSYS AIM Tutorial Flow over an Ahmed Body

Similar documents
ANSYS AIM Tutorial Turbulent Flow Over a Backward Facing Step

ANSYS AIM Tutorial Steady Flow Past a Cylinder

ANSYS AIM Tutorial Fluid Flow Through a Transition Duct

ANSYS AIM Tutorial Compressible Flow in a Nozzle

ANSYS AIM Tutorial Stepped Shaft in Axial Tension

ANSYS AIM Tutorial Thermal Stresses in a Bar

TryItNow! Step by Step Walkthrough: Spoiler Support

ANSYS AIM Tutorial Structural Analysis of a Plate with Hole

Appendix: To be performed during the lab session

Compressible Flow in a Nozzle

Supersonic Flow Over a Wedge

Simulation of Turbulent Flow over the Ahmed Body

Introduction to CFX. Workshop 2. Transonic Flow Over a NACA 0012 Airfoil. WS2-1. ANSYS, Inc. Proprietary 2009 ANSYS, Inc. All rights reserved.

Simulation of Laminar Pipe Flows

Simulation of Turbulent Flow around an Airfoil

µ = Pa s m 3 The Reynolds number based on hydraulic diameter, D h = 2W h/(w + h) = 3.2 mm for the main inlet duct is = 359

Introduction to ANSYS CFX

equivalent stress to the yield stess.

A B C D E. Settings Choose height, H, free stream velocity, U, and fluid (dynamic viscosity and density ) so that: Reynolds number

Aerodynamic Study of a Realistic Car W. TOUGERON

Heat Exchanger Efficiency

Workbench Tutorial Flow Over an Airfoil, Page 1 ANSYS Workbench Tutorial Flow Over an Airfoil

Verification of Laminar and Validation of Turbulent Pipe Flows

STAR-CCM+ User Guide 6922

Simulation of Turbulent Flow over the Ahmed Body

First Steps - Ball Valve Design

Tutorial: Simulating a 3D Check Valve Using Dynamic Mesh 6DOF Model And Diffusion Smoothing

Verification and Validation of Turbulent Flow around a Clark-Y Airfoil

NUMERICAL 3D TRANSONIC FLOW SIMULATION OVER A WING

Simulation of Turbulent Flow around an Airfoil

COMPUTATIONAL FLUID DYNAMICS USED IN THE DESIGN OF WATERBLAST TOOLING

Introduction to ANSYS FLUENT Meshing

STAR-CCM+: Wind loading on buildings SPRING 2018

Workshop 1: Basic Skills

ANSYS FLUENT. Airfoil Analysis and Tutorial

Middle East Technical University Mechanical Engineering Department ME 485 CFD with Finite Volume Method Fall 2017 (Dr. Sert)

FLUENT Secondary flow in a teacup Author: John M. Cimbala, Penn State University Latest revision: 26 January 2016

TUTORIAL#3. Marek Jaszczur. Boundary Layer on a Flat Plate W1-1 AGH 2018/2019

Flow and Heat Transfer in a Mixing Elbow

An Introduction to SolidWorks Flow Simulation 2010

Viscous Hybrid Mesh Generation

Simulation and Validation of Turbulent Pipe Flows

Module D: Laminar Flow over a Flat Plate

Visit the following websites to learn more about this book:

SolidWorks Flow Simulation 2014

Tutorial: Hydrodynamics of Bubble Column Reactors

Solved with COMSOL Multiphysics 4.2

Flow Simulation How to Handle a Vortex Across a Pressure Boundary

THE APPLICATION OF AN ATMOSPHERIC BOUNDARY LAYER TO EVALUATE TRUCK AERODYNAMICS IN CFD

Analysis of an airfoil

First Steps - Conjugate Heat Transfer

Using the Boundary Wrapper

Instructions for Muffler Analysis

Calculate a solution using the pressure-based coupled solver.

FINITE ELEMENT ANALYSIS OF A PLANAR TRUSS

Tutorial to simulate a thermoelectric module with heatsink in ANSYS

Modeling Unsteady Compressible Flow

Workshop 3: Cutcell Mesh Generation. Introduction to ANSYS Fluent Meshing Release. Release ANSYS, Inc.

Modeling Evaporating Liquid Spray

and to the following students who assisted in the creation of the Fluid Dynamics tutorials:

Express Introductory Training in ANSYS Fluent Workshop 06 Using Moving Reference Frames and Sliding Meshes

and to the following students who assisted in the creation of the Fluid Dynamics tutorials:

DrivAer-Aerodynamic Investigations for a New Realistic Generic Car Model using ANSYS CFD

BioIRC solutions. CFDVasc manual

Introduction to ANSYS FLUENT Meshing

Appendix B: Creating and Analyzing a Simple Model in Abaqus/CAE

Using Multiple Rotating Reference Frames

Workbench Tutorial Minor Losses, Page 1 Tutorial Minor Losses using Pointwise and FLUENT

EXTERNAL AERODYNAMICS

Express Introductory Training in ANSYS Fluent Workshop 02 Using the Discrete Phase Model (DPM)

5. Create two planes and split the outer cylinder volume into four quadrants using the menus

Kratos Multi-Physics 3D Fluid Analysis Tutorial. Pooyan Dadvand Jordi Cotela Kratos Team

Computational Flow Analysis of Para-rec Bluff Body at Various Reynold s Number

COMPUTATIONAL FLUID DYNAMICS ANALYSIS OF ORIFICE PLATE METERING SITUATIONS UNDER ABNORMAL CONFIGURATIONS

Tutorial: Riser Simulation Using Dense Discrete Phase Model

SMS v Simulations. SRH-2D Tutorial. Time. Requirements. Prerequisites. Objectives

MOMENTUM AND HEAT TRANSPORT INSIDE AND AROUND

Essay 5 Tutorial for a Three-Dimensional Heat Conduction Problem Using ANSYS

Modeling Flow Through Porous Media

Mesh Morphing and the Adjoint Solver in ANSYS R14.0. Simon Pereira Laz Foley

APPLIED COMPUTATIONAL FLUID DYNAMICS-PROJECT-3

ANSYS AIM 16.0 Overview. AIM Program Management

Computational Fluid Dynamics autumn, 1st week

ACTIVE SEPARATION CONTROL WITH LONGITUDINAL VORTICES GENERATED BY THREE TYPES OF JET ORIFICE SHAPE

Using Multiple Rotating Reference Frames

Verification and Validation of Turbulent Flow around a Clark-Y Airfoil

Flow Sim. Chapter 16. Airplane. A. Enable Flow Simulation. Step 1. If necessary, open your ASSEMBLY file.

Step 1: Create Geometry in GAMBIT

Wall thickness= Inlet: Prescribed mass flux. All lengths in meters kg/m, E Pa, 0.3,

RhinoCFD Tutorial. Flow Past a Sphere

Computational Simulation of the Wind-force on Metal Meshes

Modeling Evaporating Liquid Spray

Leica 3D Disto PROJECTOR in stair case

Application of Wray-Agarwal Turbulence Model for Accurate Numerical Simulation of Flow Past a Three-Dimensional Wing-body

Isotropic Porous Media Tutorial

Transition Flow and Aeroacoustic Analysis of NACA0018 Satish Kumar B, Fred Mendonç a, Ghuiyeon Kim, Hogeon Kim

Finite Element Course ANSYS Mechanical Tutorial Tutorial 4 Plate With a Hole

Repairing a Boundary Mesh

SimCafe. ANSYS WB - Airfoil - Setup (Physics) Added by Benjamin J Mullen, last edited by Benjamin J Mullen on Apr 29, :18

Hexa Meshing. Defining Surface Parameters for the Mesh Defining Edge Parameters to Adjust the Mesh Checking mesh quality for determinants and angle

Transcription:

Author(s): Sebastian Vecchi Created using ANSYS AIM 18.1 ANSYS AIM Tutorial Flow over an Ahmed Body Problem Specification Start Up Geometry Import Geometry Enclose Suppress Mesh Set Mesh Controls Generate Mesh Physics Set-Up Boundary Conditions / Forces Solution/Results Validation References

Problem Specification The Ahmed Body is a standard wind tunnel model used to represent ground vehicles. It was first defined and characterized by S.R. Ahmed in 1984 and has been used since to study the effects of drag and aspect ratio. Below is the blueprint definition of an Ahmed body. In this tutorial, we will subject an Ahmed body to air at 40 m/s in order to find the velocity vectors, pressures on the body, and streamlines around the body.

Start Up A few words on the formatting on the following instructions: 1) Notes that require you to perform an action are colored in blue 2) General information is colored in black, but does not require any action 3) Words that are bolded are labels for items found in ANSYS AIM 4) Most important notes are colored in red We are ready begin simulating in ANSYS AIM. Open ANSYS AIM by going to Start > All Apps > ANSYS 18.1 > ANSYS AIM 18.1. Once you are at the starting page of AIM, select the Fluid Flow template as shown below. You will be prompted by the Fluid Flow template to either Define new geometry, Import geometry file, or Connect to active CAD session. Select Import geometry file and press Next.

Geometry Import Geometry For this problem, we are going to import the geometry into ANSYS from a CAD package. Download the part file NewAhmed.scdoc from here. Select and open the file. Once successfully imported, press Finish. Enclose A volume needs to be created to around the Ahmed body using the enclosure feature, to represent the fluid flow area. Press Geometry in the Workflow tab and select Edit Geometry in the Geometry panel. The Enclosure tool can be found in the Analysis section of the toolbar

under the Prepare tab. Select the Ahmed body and a box will appear around the geometry. Input 500% into the Default cushion box. Uncheck the Symmetric dimensions box. Change the distance from the body to the bottom of the enclosure and distance from the midplane to the enclosure to 0m, then the distance from the front of the body to the enclosure to 2.61m. Use the picture below for guidance. Press the green checkmark and the enclosure will be generated. Suppress Now that the geometry of the flow volume has been created, we can suppress the Ahmed body from the physics calculation. Right click the Solid in the geometry tree and select Suppress for Physics.

Mesh Once you have exited the modeling window, initiate the meshing process by clicking on Mesh in the Workflow. Set Mesh Controls Under Global Sizing, change the Size function method to Curvature and proximity. The curvature option will automatically refine the mesh near the curved surfaces of the body. The proximity option will automatically refine the mesh between the bottom of the body and the ground. In the Boundary Layer Settings, under Collision avoidance, use the Layer compression setting. This will ensure continuous boundary layers around the body, which can improve accuracy for external flows.

AIM will prompt you to fix the boundary layer before generating the mesh. Click on Boundary Layer under Mesh Controls. Select the faces of the volume in contact with the Ahmed body, as shown below. The simplest way to do this is to drag a box around the Ahmed body, from the upper left to the lower right. AIM will select all faces that are completely enclosed by the box. Generate Mesh Return to the Mesh panel, then click Generate Mesh under Output or at the top of the screen by the status window for Mesh. AIM will detect that you are ready to generate the mesh and highlight the buttons in blue.

Physics Set-Up Boundary Conditions / Forces First, the inlet must be defined using the Fluid Flow Conditions. In the Add drop down menu by Fluid Flow Conditions, select Inlet. Then, using the face selection tool, define an inlet at the face upstream of the Ahmed body. The front of the body is the taller end with the rounded edges and corners. Make sure to input the Velocity magnitude as 40 m/s. Once the inlet is defined, the outlet is next. In the same Add menu, use the Outlet condition to define an outlet downstream of the body. Assign a Gauge static pressure of 0 psi.

Create openings for the sides of the flow volume by selecting Opening in the Add drop down menu. Select the top face of the flow volume, and the side face away from the Ahmed body, then input 0 Pa for the Gauge entrainment pressure.

Add a Symmetry condition from the Add drop down menu to the face of the flow volume which passes through the Ahmed body.

A Wall condition needs to be added for the remaining faces of the flow volume. In the Add menu, select Wall. AIM will automatically select all faces not already assigned.

Press Solve Physics in the Physics panel to run the calculations, then move on to the next step.

Solution/Results Press the Results button in the Workflow to extract information from the simulation. In order to find information that can be readily used, first press Evaluate Results. Once the evaluation is complete, AIM will automatically output a Velocity Vector in the Results section under Objects. Select the Velocity Vector to edit the settings with which the vectors are defined. Change Symbol distribution to Based on mesh and change At every Nth item to 4. If desired, change the Symbol sizing in the Appearance section to alter how big the arrows are. Press the Play button in the model window to see how these velocity vectors develop over time. Flow along the midplane can be visualized by displaying the velocity vectors on the symmetry plane. Change the Location to Symmetry 1, change At every Nth item to 1, and press Evaluate. Press the Play button in the model window to see how these velocity vectors develop over time.

Pressure on the Ahmed body can be plotted by adding a Contour in the Add drop down menu of the Results panel. Use Total Pressure as the Variable and then select the faces of the flow volume touching the faces of the Ahmed body.

Streamlines can also be computed, by picking the Streamline option in the Add drop down menu near the Results category. Select the faces of the Ahmed body as the Seed location. Then, change Distribution to Based on mesh and At every Nth item to 10.

Press Evaluate. If desired, change the Wire thickness in the Appearance section to alter how big the streamlines are. Press the Play button in the model window to see how these streamlines develop over time.

Validation An excellent way of validating simulations is by comparing them to research papers which are relevant. Since the Ahmed body is so widely studied and used as validation, it is not difficult to find supporting evidence. For this tutorial, the information gathered from the simulation will be compared to Embedded Large Eddy Simulation of Flow around the Ahmed Body by Domenico Caridi done in ANSYS FLUENT. Below is a contour of the pressure on the rear surface of the Ahmed body. This can be compared to our model by creating a similar contour in our simulation. Add a Contour from the Add drop down menu and select the top, side and rear faces as the Location. After changing the Variable to Pressure, the following contour plot will be created.

While qualitatively similar, the numerical results are significantly different than those found in the validation. By refining the mesh, the results can be calculated to a more accurate degree. Go back to the Mesh task in the workflow and increase the Mesh resolution all the way up. Return to the Results and press Evaluate Results, then display the Pressure contour again.

These results compare more favorably to the FLUENT results, though they are still significantly different. However, the mesh in the FLUENT study was much more refined than the one used here, especially in the critical wake region immediately behind the Ahmed body. Additional refinement of the AIM mesh would further improve the results and is recommended practice for external flow around vehicles.