Investigation of surface pressure and leading-edge vortex of slender delta wings
Abstract An overview is given of investigations on a 70° slender delta wing applying pressure-sensitive paint (PSP) and particle image velocimetry (PIV) in parallel. Experiments are conducted within the range of Reynolds number from 0.6 $$\times$$ × 106 to 1.2 $$\times$$ × 106 and angle of attack fr...
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| 主要な著者: | , , , , , , |
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| フォーマット: | Artigo |
| 言語: | Inglês |
| 出版事項: |
SpringerOpen
2026-04-01
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| シリーズ: | Advances in Aerodynamics |
| 主題: | |
| オンライン･アクセス: | https://doi.org/10.1186/s42774-025-00242-3 |
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