ANSYS Fluent Tutorial | Airfoil Simulation of Subsonic, Transonic & Supersonic Flow! скачать в хорошем качестве

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. 👉 Don’t forget to like, share, and subscribe for more COMSOL and ANSYS tutorials! 📌 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. 🌐 Explore More: 🔗 https://arminhashemi.org/ 🛠️ Need Help with a Project? 📩 https://arminhashemi.org/order-project/ 📸 Follow Me on Instagram:   / caewitharminhashemi   💼 Connect on LinkedIn:   / cae-with-armin   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 #ansys #ansysfluent #supersonic #subsonic #caewitharmin #SupersonicFlow