Preliminary Study of Aerodynamic Performance for Waverider-based Hypersonic Vehicles with Dorsal Mounted Engines
文献类型:会议论文
作者 | Xiao Y(肖尧)![]() ![]() ![]() |
出版日期 | 2017 |
会议日期 | 6-9 March 2017 |
会议地点 | Xiamen, China |
关键词 | Aerodynamics Air Engines Aspect Ratio Computational Fluid Dynamics Drag Engines Hypersonic Aerodynamics Lift Lift Drag Ratio Propulsion Spacecraft Vehicles |
英文摘要 | To aim at improving the aerodynamic performance of hypersonic air-breathers, a family of novel waverider-based configurations which integrating two dorsal mounted engines are proposed. The key feature of this type of configurations is that the lower surface of the vehicle could fully preserve the characteristics of waveriders, thus it is conducive to enhance the lift-to-drag ratio effectively. Basic waveriders of configurations are obtained by using a method that generating waverider as two parts which are defined by the leading edge and the trailing edge respectively. The forebody of the vehicle is designed by rotating and assembling two waverider-based-surfaces, which are the front part of basic waveriders. A group of conceptual configurations with different aspect ratio is presented. Computational Fluid Dynamics is employed to evaluate the aerodynamic performance. The results demonstrate that the maximum lift-to-drag ratio of configurations is greater than 5 in viscous condition, meanwhile, the forebody could produce a good quality flowfield for the propulsion system. 漏 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. |
会议录 | 21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017
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会议录出版者 | American Institute of Aeronautics and Astronautics Inc, AIAA |
会议录出版地 | USA |
语种 | 英语 |
URL标识 | 查看原文 |
ISBN号 | 978-1-62410-463-3 |
源URL | [http://dspace.imech.ac.cn/handle/311007/72192] ![]() |
专题 | 力学研究所_高温气体动力学国家重点实验室 |
作者单位 | 1.State Key Laboratory of High-Temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences, Beijing 2.190, China (2) School of Engineering Science, University of Chinese Academy of Sciences, Beijing 3.100049, China |
推荐引用方式 GB/T 7714 | Xiao Y,Cui K,Li GL,et al. Preliminary Study of Aerodynamic Performance for Waverider-based Hypersonic Vehicles with Dorsal Mounted Engines[C]. 见:. Xiamen, China. 6-9 March 2017. |
入库方式: OAI收割
来源:力学研究所
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