Compressible Flow Simulation Around an Airplane Wing
In this tutorial learn how to:
Set up and run a steady-state compressible simulation over an airplane wing
Extract fluid volume using CAD mode
Initialize velocity and temperature across the domain
Create and assign topological entity sets to boundary conditions
Mesh using the standard algorithm in SimScale and assess mesh quality
Explore SimScale’s online post-processor to analyze the results
Links:
Import tutorial: https://hubs.la/Q01p4j3r0
Documentation: https://hubs.la/Q01p4jpX0
---Contents-------------------------------
00:00 - Introduction
01:09 - Cad Model
01:29 - Flow Volume Extraction
05:22 - Create Simulation
06:16 - Global Settings
06:54 - Material Assignment
07:32 - Boundary Conditions
14:35 - Initial Conditions
15:54 - Numerics & Simulation Control
17:45 - Result Control
19:46 - Mesh Setup
24:56 - Simulation Run
25:40 - Mesh Quality Assessment
28:52 - Solver Log and Plots
31:36 - Post-Processing
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