Ansys Cfd For Turbulent Aerodynamics Flows
Last updated 2/2019
MP4 | Video: h264, 1280x720 | Audio: AAC, 44.1 KHz
Language: English | Size: 1.11 GB | Duration: 1h 45m
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...
Read more
Continue reading...