NACA 0015 airfoil aerodynamics validation using Ansys Fluent

This is a detailed CFD simulation process for aerodynamics study of NACA 0015 airfoil in Ansys Fluent. The simulation results are validated with the experimental and reference data.

What does this package include

1. Detailed step-by-step instructions of the complete simulation process form geometry to validation

2. Airfoil coordinate file for geometry import in Space claim

3. Post processing excel sheet for validation

4. Technical support related to the steps mentioned in the process document

This Simulation process is created using the Ansys Fluent version 2024R2.It is expected to work 

in older versions with no or minimal changes.

You can reach out to us for any help related to software version issues. 

Cost of this package is INR 500 + GST as applicable

Write an email at enquiry@integralcae.com for further payment instructions. This is to ensure a 

secure payment process and compliance.

Upon successful payment, the simulation process package will be sent via email.