ANSYS Fluent Tutorial | Airfoil Simulation of Subsonic, Transonic & Supersonic Flow!
In "*ANSYS Fluent Tutorial | Airfoil Simulation of Subsonic, Transonic & Supersonic Flow!*"
step-by-step ANSYS Fluent tutorial, we’ll model the flow regime around a NACA 2415 airfoil in a 2D compressible domain. The video covers the setup of subsonic, transonic, and supersonic flows, along with the effects of pressure and temperature changes, and we will see bow shock, normal shock, and oblique shock in the flow regimes!
🔍 What you’ll learn in this video:
✅ Import a NACA 2415 airfoil geometry from a text file
✅ Create the CFD domain and apply Pressure Far-Field boundary conditions
✅ Use ideal gass with sutherland viscosity model
✅ Add mesh refinement zones for higher accuracy
✅ Enable Energy Equation and k-omega SST turbulence model
This tutorial is perfect for students, researchers, and engineers interested in aerodynamics and CFD simulations.
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📌 Keywords: ANSYS Fluent airfoil simulation, CFD tutorial, NACA airfoil, compressible flow, supersonic shock waves, turbulence modeling, k-omega SST, mesh refinement, subsonic vs supersonic flow.
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0:00 4:51 Introduction
4:52 6:57 Airfoil text file
6:58 15:46 Geometry
15:47 19:55 Mesh
19:56 23:52 Setup
23:53 25:01 Transonic Results
25:02 27:00 Supersonic Results
27:01 Subsonic Results
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