Fuel Tank Vertical Sloshing during Aircraft Landing
In this article, the influence of the fuel sloshing on the tank under the landing condition is investigated to explain the skin deformation of wing tank. Based on the SPH method, a simplified fuel tank model of gas-liquid-solid three-phase is established. NanoFluidX, a fluid dynamics simulation tool...
| Format: | Article |
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| Language: | zho |
| Published: |
EDP Sciences
2020-04-01
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| Series: | Xibei Gongye Daxue Xuebao |
| Subjects: | |
| Online Access: | https://www.jnwpu.org/articles/jnwpu/full_html/2020/02/jnwpu2020382p288/jnwpu2020382p288.html |