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Author(s): Sebastian Vecchi, ANSYS Inc.
Problem Specification
1. Start-Up
2. Geometry
3. Mesh
4. Physics Setup
5. Results
6. Verification & Validation
Compressible Flow Over an Airfoil
Created using ANSYS 18.1
Problem Specification
A wing with a NACA 0012 airfoil section has a chord of 1 meter, a span of 1 meter, and a thickness of 0.01 meter. The wing is made of Aluminum 6061-T6. If air moves at 987.84 km/hour around the airfoil, find the velocity vectors of compressible flow over the airfoil.
