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《材料导报》期刊社  2017, Vol. 31 Issue (4): 131-136    https://doi.org/10.11896/j.issn.1005-023X.2017.04.028
  计算模拟 |
高孔隙率多孔氮化硅构件较高马赫数下流-热-固耦合力学特性分析*
张晨1, 应国兵1, 王乘1, 王鹏举1, 田宝娜1, 韩建兴2, 王香2
1 河海大学力学与材料学院, 南京 211100;
2 哈尔滨工程大学材料科学与化学工程学院, 哈尔滨 150001
Analyzing the Fluid-Solid-Heat Coupled Mechanical Properties of Highly
Porous Silicon Nitride Member Under High Mach Number
ZHANG Chen1, YING Guobing1, WANG Cheng1, WANG Pengju1, TIAN Baona1,
HAN Jianxing2, WANG Xiang2
1 College of Mechanics and Materials, Hohai University, Nanjing 211100;
2 College of Materials Science and Chemical Engineering, Harbin Engineering University, Harbin 150001
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摘要 以凝胶注模技术制备的固相含量为40%、45%、50%(质量分数,下同),孔隙率高达65.24%、63.26%、61.19%的多孔氮化硅天线罩材料作为研究对象。将测得的材料性能参数作为有限元分析模拟的数据支撑,构件模型载体选择正切尖拱形,使用FLUENT模拟流场,结构场采用ANSYS软件,热力耦合得到不同固相含量的材料在不同马赫数下流-热-固耦合后的热应力强度,对其力学特性进行分析。结果表明,较高马赫数下的飞行构件的尾部连接端是受热应力最大的部位,也是失稳较为严重的部位。飞行构件的结构稳定性需通过加固尾部连接端来提高;气动热是引起天线罩构件失稳的首要问题,解决结构失稳的关键在于解决气动热,可通过在天线罩构件外增加耐热隔层,使其免受气动热;多孔氮化硅材料的孔隙率与失稳时对应的马赫数成正比,热导率是影响多孔氮化硅天线罩构件在较高马赫数下受到热应力大小的关键因素。
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张晨
应国兵
王乘
王鹏举
田宝娜
韩建兴
王香
关键词:  高孔隙率  多孔氮化硅  较高马赫数  流-热-固耦合  力学特性    
Abstract: The 40%, 45% and 50% (mass fractionm) solid content porous silicon nitrides with porosity of 65.24%, 63.26% and 61.19%, respectively, were successfully fabricated by gel-casting. And the gel-cast porous silicon nitride flight member with tangent pointed arch model was investigated by finite element analysis, using the property parameters as calculating data. The flow field was simulated by FLUENT software, and the fluid-solid-heat coupling analysis under different Mach number was conducted by ANSYS calculation. It was found that the tail connection end of the component was subjected to the maximum stress and exhibited serious instability. The stability of the component needed to be enhanced by strengthening the tail connection end. The pneumatic heat was the key to the instability of the component. It was revealed that an outside heat insulation layer was needed to protect the member under high Mach number. The porosity of porous silicon nitride material was in direct proportion to that of the Mach number at unstable situation. The thermal conductivity of porous silicon nitride was the key to the value of thermal stress under high Mach number.
Key words:  high porosity    porous silicon nitride    high Mach number    fluid-solid-heat coupling    mechanical property
               出版日期:  2017-02-25      发布日期:  2018-05-02
ZTFLH:  TB122  
基金资助: *总装预研教育部支持计划;总装预研基金;国家自然科学基金(11302068);中央高校基本业务费(2013B04914;2015B21814);中国博士后科学基金(2014T70465;2013M531261)
通讯作者:  应国兵:通讯作者,男,1983年生,博士,副教授,研究方向为工程力学材料应用 E-mail:yingg62010@126.com   
作者简介:  张晨:男,1990年生,硕士研究生,研究方向为工程力学仿真模拟 E-mail:zhangchh2015@126.com
引用本文:    
张晨, 应国兵, 王乘, 王鹏举, 田宝娜, 韩建兴, 王香. 高孔隙率多孔氮化硅构件较高马赫数下流-热-固耦合力学特性分析*[J]. 《材料导报》期刊社, 2017, 31(4): 131-136.
链接本文:  
http://www.mater-rep.com/CN/10.11896/j.issn.1005-023X.2017.04.028  或          http://www.mater-rep.com/CN/Y2017/V31/I4/131
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