Ansys Cfd For Turbulent Aerodynamics Flows

You will learn about the aerodynamic flows CFD using Ansys ICEMCFD and Ansys Fluent

What you'll learn
You will be able to create airfoil data file from coordinates for ICEMCFD
You will be to create high quality hexa mesh with boundary layer and Y+ considerations
How to create three meshes for mesh-independence study
Requirements
Basic knowledge of CFD is preferable but not compulsory
Minimum Specs: Computer with 4GB RAM and i3 processor
Description
In this course you will learn about the CFD of external aerodynamics. In this course first we will create geometry of airfoil in ICEMCFD and then we will create high quality hexa mesh. After that we will solve this case in Fluent.  You will run case at angle of attack zero and angle of attack 10 and compare results with NASA data for Cp, lift coefficient and drag coefficient. In future we will introduce more complex problems. Hope to see you soon on course.

Overview

Section 1: Introduction

Lecture 1 Introduction to course

Section 2: Flow equations, Turbulence modeling and Y+

Lecture 2 Introduction to flow equations and turbulence

Lecture 3 Turbulence models

Section 3: Workshop 1 : Geometry and Hexa mesh generation in ICEMCFD Hexa

Lecture 4 Introduction to workshop 1

Lecture 5 Importing NACA 0012 coordinates into ICEMCFD

Lecture 6 Domain and parts

Lecture 7 Blocking, association and C-grid generation

Lecture 8 Premesh settings and generation of premesh of coarse mesh

Lecture 9 Mesh quality, mesh export, meshes for mesh independece study

Section 4: WS2 : Fully turbulent CFD analysis of NACA0012 Airfoil

Lecture 10 Introduction

Lecture 11 Setting up case in Fluent

Lecture 12 Post processing results at zero angle of attack (AoA)

Lecture 13 Drag coefficient at AoA = 0 and 10 deg - Experimental vs CFD and discussion

Lecture 14 Coefficient of pressure at AoA = 0 and 10 deg along with Y+ plots

Lecture 15 Plotting CFD Cp (coefficient of pressure) plot in excel

Lecture 16 Digitizing experimental Cp plot and comparing with CFD Cp in Excel

Any one who is interested to learn ICEM CFD hexa meshing at beginner level