Volume 28 Issue 7
Jul.  2013
Turn off MathJax
Article Contents
CHENG Xing-hua, YANG Tao, FENG Zhi-wei. Analysis of aeroheating-temperature field coupling characteristics for thermal protection panel of quasi-wavrider[J]. Journal of Aerospace Power, 2013, 28(7): 1591-1597.
Citation: CHENG Xing-hua, YANG Tao, FENG Zhi-wei. Analysis of aeroheating-temperature field coupling characteristics for thermal protection panel of quasi-wavrider[J]. Journal of Aerospace Power, 2013, 28(7): 1591-1597.

Analysis of aeroheating-temperature field coupling characteristics for thermal protection panel of quasi-wavrider

  • Received Date: 2012-07-10
  • Publish Date: 2013-07-28
  • For thermal protection panel of quasi-waverider, the loose coupling algorithm was applied to drive the iteration of the aeroheating and heat transfer analysis. Then, the coupling characteristics of aeroheating-temperature field were studied. The results show that, before radiative equilibrium, the errors of cold wall and radiative equilibrium aeroheating are +55.1% and -15.4% over actual aeroheating respectively, so coupling analysis for aeroheating-temperature field was required. As the local adiabatic wall temperature is not changed with time, the surface heat-transfer coefficient is a key parameter for coupling effect. Only two aeroheating calculations are needed during calculation of coupling aeroheating-temperature field with average heat convection coefficient, and the error of predicted wall temperature is less than 2.5%, thus highly improving the analysis efficiency of coupled aeroheating-temperature field.

     

  • loading
  • [1]
    宋少云.多场耦合问题的协同求解方法研究与应用 [D].武汉:华中科技大学,2007. SONG Shaoyun. Research and application of collaborative solution method for multiphysics problems [D].Wuhan: Huazhong University of Science and Technology,2007.(in Chinese)
    [2]
    Mcnamara J J,Friedmann P P,Powell K G,et al.Three-dimensional aeroelastic and aero-thermoelastic behavior in hypersonic flow.AIAA-2005-2175,2005.
    [3]
    Culler A J,Mcnamara J J.Studies on fluid-thermal-structural coupling for aerothermoelasticity in hypersonic flow[J].AIAA Journal 2010,48(8):1721-1738.
    [4]
    Spain C,Soistmann D,Parker E.An overview of selected NASP aeroelastic studies at the NASA Langley Research Center.AIAA 90-25218,1990.
    [5]
    吴志刚,惠俊鹏,杨超.高超声速下翼面的热颤振工程分析[J].北京航空航天大学学报,2005,31(3):270-273. WU Zhigang,HUI Junpeng,YANG Chao.Hypersonic aerothermoela stic analysis of wings[J].Journal of Beijing University of Aeronautics and Astronautics,2005,31(3):270-273.(in Chinese)
    [6]
    吕继航,杨茂,陈凤明.超音速舵面热气动弹性仿真[J].计算机仿真,2010,27(3):43-46. LV Jihang,YANG Mao,CHEN Fengming.Aerothermoelastic simulation of supersonic missile rudder[J].Computer Simulation,2010,27(3):43-46.(in Chinese)
    [7]
    Borrelli R,Riccio A,Tescione D,et al.Thermo-structural behaviour of an UHTC made nose cap of a reentry vehicle[J].Acta Astronautica,2009,65(314):441-456.
    [8]
    Myers D E,Martin C J,Blosser M L.Parametric weight comparison of advanced metallic,ceramic tile,and ceramic blanket thermal protection systems.NASA/TM-2000-210289,2000.
    [9]
    中国人民解放军总装备部军事训练教材编辑工作委员会.高超声速气动热和热防护[M].北京:国防工业出版社,2003.
    [10]
    Fay J A,Riddell F R.Theory of stagnation point heat transfer in dissociated air[J].Journal of the Aerospace Science,1985,25(2):73-85.
    [11]
    黄志澄.高超声速飞行器空气动力学[M].北京:国防工业出版社,1995.
    [12]
    吕丽丽,张伟伟,叶正寅.高超声速再入体表面热流计算[J].应用力学学报,2006,23(2):259-263. LV Lili,ZHANG Weiwei,YE Zhengyin.The calculation of surface heating rates for hypersonic reentry-body[J].Chinese Journal of Applied Mechanics,2006,23(2):259-263.(in Chinese)
    [13]
    程兴华,杨涛,常中东.熵层对高超声速二维钝楔气动参数的影响[J].航空动力学报,2012,27(6):1362-1367. CHENG Xinghua,YANG Tao,CHANG Zhongdong.Influence of entropy layer on aerodynamics parameters for hypersonic 2-D blunt wedge[J].Journal of Aerospace Power,2012,27(6):1362-1367.(in Chinese)
    [14]
    CHENG Xinghua,YANG Tao,LIU Xin.An improved data exchange algorithm based on the relationships between point and triangle[J].Advanced Materials Research,2012,538/539/540/541:777-783.
    [15]
    Cebral J R,Loehner R.Fluid-structure coupling extensions and improvements [R].AIAA 97-0858,1997.
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (1624) PDF downloads(1140) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return