高超声速飞行器流-热-固耦合数值模拟

doi:10.11949/j.issn.0438-1157.20150284

化工学报 ›› 2015, Vol. 66 ›› Issue (S1): 89-94.DOI: 10.11949/j.issn.0438-1157.20150284

高超声速飞行器流-热-固耦合数值模拟

陈梅洁, 程珙, 田枫林, 何玉荣

哈尔滨工业大学能源科学与工程学院, 黑龙江哈尔滨 150001

收稿日期:2015-03-09 修回日期:2015-03-14 出版日期:2015-06-30 发布日期:2015-06-30
通讯作者: 何玉荣
基金资助:
国家自然科学基金创新研究群体项目(51121004)。

Hypersonic vehicle flow-heat-solid coupling simulation

CHEN Meijie, CHENG Gong, TIAN Fenglin, HE Yurong

School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, Heilongjiang, China

Received:2015-03-09 Revised:2015-03-14 Online:2015-06-30 Published:2015-06-30
Supported by:
supported by the Foundation for Innovative Research Groups of the National Natural Science Foundation of China (51121004).

摘要/Abstract

摘要：

选用HiFire-1锥体部分作为研究对象, 采用顺序耦合方法, 对飞行器锥体的流-热-固耦合场进行了研究分析。在外流场的数值模拟中采用Transition k-kl-w湍流模型准确计算出了转捩位置和热流数值, 在温度场和应力场的数值模拟中计算了气动加热1 s时温度场和应力场的分布, 温度最高点和变形最大处均出现在头锥顶端, 温度在轴线方向上呈现环状的分布, 沿轴线逐渐降低, 整体结构的弹性变形和温度正相关, 且主要变形区域集中在前端高温区。

关键词: 高超声速, 流-热-固耦合, HiFire-1锥体, 湍流模型, 数值模拟

Abstract:

Take the HiFire-1 cone as the research subject to analyze the aircraft flow-heat-solid coupling field by sequential coupling method. Transition k-kl-w turbulence model has been used to accurately calculate the position of the transition and flux values in the outside flow field numerical simulation which is basically consistent with the experimental data. In temperature field and stress field numerical simulation, the temperature field and stress field distribution of the HiFire-1 cone is calculated when aerodynamic heating time is 1 s. The results showed that the maximum temperature and deformation point occurred at the top of the cone. Cone temperature presented cyclic distribution in the axial direction, and decreased gradually along the axis. The top node temperature gradually rises over time and the change trend gradually slows down. The elastic deformation of the overall structure is positive correlation with the temperature, and the main deformation zone focus on the front area of high temperature.

Key words: hypersonic, flow-heat-solid coupling, HiFire-1 cone, turbulence model, numerical simulation

中图分类号:

TQ025.1

陈梅洁, 程珙, 田枫林, 何玉荣. 高超声速飞行器流-热-固耦合数值模拟[J]. 化工学报, 2015, 66(S1): 89-94.

CHEN Meijie, CHENG Gong, TIAN Fenglin, HE Yurong. Hypersonic vehicle flow-heat-solid coupling simulation[J]. CIESC Journal, 2015, 66(S1): 89-94.

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高超声速飞行器流-热-固耦合数值模拟

Hypersonic vehicle flow-heat-solid coupling simulation

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