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Author: Benjamin Mullen, Cornell University

Problem Specification
1. Pre-Analysis & Start-Up
2. Geometry
3. Mesh
4. Setup (Physics)
5. Solution
6. Results
7. Verification & Validation
8. Exercises

In this tutorial, we will show you how to use FLUENT to simulate the flowfield over a wedge "flying" at Mach 3 in atmospheric pressure at 300 Kelvin.

A uniform supersonic stream encounters a wedge with a half-angle of 15 degrees as shown in the figure below.

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The stream is at the following conditions:

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Go to Step 1 - Pre-Analysis & Start-Up