NACA0012 Airfoil, Compressible Flow, Paper Validation
Price: $96
In this project, we intend to simulate the NACA0012 airfoil with the compressible flow around it to compare and validate the results with the results in the article.
NACA0012 Airfoil, Compressible Flow, Paper Validation
Price: $96
In this project, we intend to simulate the NACA0012 airfoil with the compressible flow around it to compare and validate the results with the results in the article.
NACA0012 Airfoil (Compressible Flow), Paper Numerical Validation, ANSYS Fluent CFD Simulation training
In this project, We simulated the compressible flow around the NACA0012 airfoil by Ansys Fluent Software. Then we compared the results with the results extracted from an article called this "Numerical Simulation OF VISCOUS TRANSONIC AIRFOIL FLOWS".
Geometry & Mesh
The geometry is designed by the design modeler Software.
The meshing of this present model has been generated by ANSYS Meshing software. The mesh grid is structured, and the total cell number is 73320.
NACA0012 Airfoil CFD Simulation
To simulate the present model, several assumptions are considered, which are:
- The solver is density-based due to compressibility.
- Simulation has been done as Steady State
- We ignored the gravity effect.
Paper Validation Results
By comparing the simulation results with the results in the article, it can be concluded that the simulation has been validated by the article.
| Coef. | Experimental Value | CFD Value |
| CD | 0.0079 | 0.00804 |
| CL | 0.241 | 0.246 |
