Numerical investigation of the compressible flow past an aerofoil
Numerical investigation of the compressible flow past an 18% thick circular-arc aerofoil was carried out using detached-eddy simulation for a free-stream Mach number M? = 0.76 and a Reynolds number Re = 1.1 × 107. Results have been validated carefully against experimental data. Various fundamental m...
| Main Authors: | , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
2010-12-17.
|
| Subjects: | |
| Online Access: | Get fulltext |