Set up your own cloud-native simulation in minutes.Start Simulating Now

NACA 0012 Airfoil CFD Analysis (H.B) - Copy

Open Project
Copy Project
NACA 0012 Airfoil CFD Analysis (H.B) - Copy image
views 51shares 0
v1rtu4l702
Created

Last modified

Statistics
geometries 1 Geometrymeshes 3 Meshessimulations 2 Simulation setupsruns 2 Results

About this project

In this project we examined the Effect of Boundary Layers on the NACA 0012 Airfoil. In-compressible fluid flow simulation is selected for the project. Free stream velocity is selected as 10 m/s having A.O.A 10 with the airfoil. - Copy

Share this project

Related Projects

airflow_around_a_spoiler_1 image
Tutorial - Airflow around a spoiler

by Ali_ArafatAli_Arafat


Project History

  • HamzaBaig

    HamzaBaig created this project

  • v1rtu4l702

    v1rtu4l702 copied this project