Summary

Introduction

I. Study configuration
1. Physical description
2. Inflow Boundary Conditions

II. Manual
1. Preprocessing
2. Solving
3. Postprocessing

III. Transonic flow
1. Mach 0.2
2. Mach 0.5
3. Mach 0.8

IV. Supersonic flow
1. Modified linear profile
2. Upwind difference

Conclusion