I am excited to share the results of my recent computational fluid dynamics (CFD) simulation using Large Eddy Simulation (LES) to analyze vortex shedding on a NACA 4412 airfoil. The simulation was conducted at a Mach number of 0.09 and an angle of attack of 13.87 degrees. In this study, LES provided detailed insights into the turbulent flow structures and vortex dynamics around the airfoil. The video below demonstrates the complex flow patterns and the shedding vortices that occur at these conditions. This analysis is crucial for understanding the aerodynamic performance and potential noise generation mechanisms of airfoils in various applications. Feel free to reach out if you have any questions or would like to discuss the findings further! #CFD #LES #Aerodynamics #NACA4412 #VortexShedding #AerospaceEngineering
Very informative
Congratulations on your recent CFD simulation work, Caner! It's impressive to see the detailed insights you've gained into turbulent flow structures and vortex dynamics. Could you share more about the specific applications where understanding these vortex dynamics can significantly impact performance or noise reduction? Looking forward to discussing your findings further!
Congratulations on a beautiful and useful study. It has proven beneficial for visualizing eddies in the turbulence spectrum and for aero-acoustic research. I look forward to your next work with great anticipation!!
Senior Aerodynamics Design Specialist
6moFantastic work! The detailed visualization of vortex shedding at such specific conditions is truly impressive. I'm curious about the computational resources and time required for this LES simulation. Could you provide some insights on that?