Computational study of a battle damaged finite aspect ratio wing
Numerical studies have been carried out on a battle damaged NACA 641-412 half wing of aspect ratio 8.2 at a Reynolds number of 5.5 x 105. The simulated gunfire damage was represented by a single hole with a diameter of 0.2 wing chord. The hole was centred at half chord and at spanwise locations of 4...
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| Main Authors: | , , |
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| Format: | Default Conference proceeding |
| Published: |
2012
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| Subjects: | |
| Online Access: | https://hdl.handle.net/2134/10068 |
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