高超声速钝锥体热环境仿真计算
Simulation Calculation of Thermal Environment for Hypersonic Blunt Cone
Received date: 2018-03-30
Online published: 2025-05-29
张超 , 刘洪泉 , 赵泽华 , 王记妃 , 胡东阳 , 张玺 , 翟北北 . 高超声速钝锥体热环境仿真计算[J]. 弹箭与制导学报, 2018 , 38(6) : 43 -46 . DOI: 10.15892/j.cnki.djzdxb.2018.06.010
With the development requirement of the aircraft at higher speed and longer distance, the aerodynamic heating problem becomes more and more serious. Based on ANSYS software, the ball head blunt cone in a typical body is taken as the calculation model for calculation of thermal environment in flight conditions. A complete numerical solution method is established. It is verified that ANSYS software can effectively solve the problem of aerodynamics. And the convection field, the temperature field, and the structural field characteristics have been studied, providing a reliable reference and analysis to the thermal design and optimization.
Key words: aerodynamic heating; ANSYS; ball head blunt cone; numerical solution; thermal design
| [1] | 李会萍. 高超声速飞行器气动加热特性及其计算方法研究[D]. 上海: 上海交通大学, 2010. |
| [2] | CLEARY J W. Effects of angle of attack and bluntness on laminar heating rate distribution of a 15° cone at a mach number of 10.6: NASA-TND-5450[R]. [S. l.: s. n.], 1969. |
| [3] | 陆应龙. 基于NS方程的飞行器气动力气动热数值研究[D]. 上海: 上海交通大学, 2014. |
| [4] | 张胜涛, 陈方, 刘洪. 基于多场耦合的飞行器热环境数值分析方法研究[J]. 空气动力学学报, 2014, 32(6): 861-867. |
| [5] | 翟章华, 刘伟, 曾明, 等. 高超声速空气动力学[M]. 长沙: 国防科技大学出版社, 2001: 100-103,130-132. |
| [6] | 王杰. 高超声速飞行器气动加热计算技术[D]. 南京: 南京航空航天大学, 2012. |
| [7] | 贺国宏, 高晓成, 庞勇. 钝体高超声速气动加热与结构热传递耦合的数值计算[J]. 空气动力学学报, 2001, 19(2): 177-485. |
| [8] | 夏刚, 刘新建, 程文科, 等. 钝体高超声速气动加热与结构热传递耦合的数值计算[J]. 国防科技大学学报, 2003, 25(1): 35-39. |
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