3D Transonic Flow Over a Wing
Modeling Objectives & Problem Description - Lesson 1
Start-up & Pre-Analysis - Lesson 2
Geometry - Lesson 3
5 Topics
Importing the Geometry
Creating the Flow Domain
Creating Body of Influence Geometry
Splitting Wing Face
3D Wing Geometry Creation (optional)
Meshing - Lesson 4
2 Topics
Sizing the Mesh
Mesh Quality and Adding Named Selections
Physics Set-up - Lesson 5
2 Topics
Choosing the Model
Setting the Boundary Conditions
Numerical Solution - Lesson 6
Numerical Results - Lesson 7
8 Topics
Examining lift and drag
Looking at the Pressure and Mach Number Distribution
Investigating the Boundary Layer
Looking at Trailing Edge Vortices
Plotting and Comparing the Pressure Coefficient
Visualizing Vorticity
Pressure Contours Animation
Creating an Animation (optional)
Verification & Validation - Lesson 8
2 Topics
Verification
Validation
Post Completion Survey
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Investigating the Boundary Layer
3D Transonic Flow Over a Wing
Numerical Results - Lesson 7
Investigating the Boundary Layer
Summary of the above video:
Create Contours of Mach Number on Symmetry Plane
Turn on Pressure Coefficient Contours on Symmetry Plane
View Divisions of contours: Mach Contours → Render → Constant Coloring
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