| Configuration optimization of hypersonic vehicles under transitional flow conditions | |
Sun QH(孙泉华) ; Fan J(樊菁); Jiang JZ(蒋建政); Cui K(崔凯); Sun QH(孙泉华)
| |
| Source Publication | 16th AIAA/DLR/DGLR International Space Planes an Hypersonic Systems and Technologies Conference.Germany, Bremen.2009-10. |
| 2009-12-28 | |
| Conference Name | 16th AIAA/DLR/DGLR International Space Planes an Hypersonic Systems and Technologies Conference |
| Conference Date | 2009-10 |
| Conference Place | Germany, Bremen |
| Abstract | The rarefied gas effects on several configurations are investigated under hypersonic flow conditions using the direct simulation Mont Carlo method. It is found that the Knudsen number, the Mach number, and the angle of attack all play a mixed role in the aerodynamics of a flat plate. The ratio of lift to drag decreases as the Knudsen number increases. Studies on 3D delta wings show that the ratio of lift to drag could be increased by decreasing the wing thickness and/or by increasing the wing span. It is also found that the waveriders could produce larger ratio of lift to drag as compared with the delta wing having the same length, wing span, and cross section area. |
| Indexed By | EI |
| Language | 中文 |
| Document Type | 会议论文 |
| Identifier | http://dspace.imech.ac.cn/handle/311007/32987 |
| Collection | 高温气体动力学国家重点实验室 |
| Corresponding Author | Sun QH(孙泉华) |
| Recommended Citation GB/T 7714 | Sun QH,Fan J,Jiang JZ,et al. Configuration optimization of hypersonic vehicles under transitional flow conditions[C]16th AIAA/DLR/DGLR International Space Planes an Hypersonic Systems and Technologies Conference.Germany, Bremen.2009-10.,2009. |
| Files in This Item: | Download All | |||||
| File Name/Size | DocType | Version | Access | License | ||
| AIAA-185337-453.pdf（377KB） | 会议论文 | 开放获取 | CC BY-NC-SA | View Download | ||
Items in the repository are protected by copyright, with all rights reserved, unless otherwise indicated.
Edit Comment