ANSYS CFD for Turbulent Aerodynamics Flows
Training
Online
Description
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Type
Training
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Methodology
Online
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Class hours
2h
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Start date
Different dates available
"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. "
Facilities
Location
Start date
Start date
About this course
"You will be able to create airfoil data file from coordinates for ICEMCFDYou will be to create high quality hexa mesh with boundary layer and Y+ considerationsHow to create three meshes for mesh-independence study"
Any one who is interested to learn ICEM CFD hexa meshing at beginner level
"Basic knowledge of CFD is preferable but not compulsoryMinimum Specs: Computer with 4GB RAM and i3 processor"
"-100% online -Access to the course for life -30 days warranty money back -Available from desktop or mobile app -Can begin and finish the course any time -Can repeat the course any times"
Reviews
This centre's achievements
All courses are up to date
The average rating is higher than 3.7
More than 50 reviews in the last 12 months
This centre has featured on Emagister for 3 years
Subjects
- Geometry
- Quality Training
- Ansys
- CFD
- ICEMCFD
- CFD Software
- Aerodynamic
- Airfoil
- Mesh
- Hexa
- Hexa mesh
- C-GRID
- Turbulence models
- Flows
- Ansys fluent
- NASA
- Equations
- Turbulence
- NASA data
- Hexa Mesh generation
Course programme
Introduction to course
Flow equations, Turbulence modeling and Y+
Introduction to flow equations and turbulence
Turbulence models
Workshop 1 : Geometry and Hexa mesh generation in ICEMCFD Hexa
Introduction to workshop 1
Importing NACA 0012 coordinates into ICEMCFD
Domain and parts
Blocking, association and C-grid generation
Premesh settings and generation of premesh of coarse mesh
Mesh quality, mesh export, meshes for mesh independece study
WS2 : Fully turbulent CFD analysis of NACA0012 Airfoil
Introduction
Setting up case in Fluent
Post processing results at zero angle of attack (AoA)
Drag coefficient at AoA = 0 and 10 deg - Experimental vs CFD and discussion
Coefficient of pressure at AoA = 0 and 10 deg along with Y+ plots
Plotting CFD Cp (coefficient of pressure) plot in excel
Digitizing experimental Cp plot and comparing with CFD Cp in Excel"
ANSYS CFD for Turbulent Aerodynamics Flows