Authors: Lara Backer and Rajesh Bhaskaran, Cornell University
Problem Specification
1. Pre-Analysis & Start-Up
2. Geometry
3. Mesh
4. Physics Setup
5. Numerical Solution
6. Numerical Results
7. Verification & Validation
Exercises
Comments
Exercises
The user defined function downloaded in the first section is only applicable to cylindrical boundaries due to the definition of the lift function as a function of theta. Alter the UDF to be applicable to any surface geometry, such as an airfoil, and verify that it calculates the same value for the cylinder as the UDF for this section.
Solution file (UDF for any surface geometry): here