留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

喷流干扰气动热数值模拟的若干影响因素

林博希 阎超 李亚超

林博希, 阎超, 李亚超等 . 喷流干扰气动热数值模拟的若干影响因素[J]. 北京航空航天大学学报, 2016, 42(6): 1210-1218. doi: 10.13700/j.bh.1001-5965.2015.0379
引用本文: 林博希, 阎超, 李亚超等 . 喷流干扰气动热数值模拟的若干影响因素[J]. 北京航空航天大学学报, 2016, 42(6): 1210-1218. doi: 10.13700/j.bh.1001-5965.2015.0379
LIN Boxi, YAN Chao, LI Yachaoet al. Some influence factors in aerodynamic heat transfer numerical simulation of jet-interaction flow[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(6): 1210-1218. doi: 10.13700/j.bh.1001-5965.2015.0379(in Chinese)
Citation: LIN Boxi, YAN Chao, LI Yachaoet al. Some influence factors in aerodynamic heat transfer numerical simulation of jet-interaction flow[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(6): 1210-1218. doi: 10.13700/j.bh.1001-5965.2015.0379(in Chinese)

喷流干扰气动热数值模拟的若干影响因素

doi: 10.13700/j.bh.1001-5965.2015.0379
详细信息
    作者简介:

    林博希 男,博士研究生。主要研究方向:计算流体力学。E-mail:boxilin@buaa.edu.cn;阎超 男,博士,教授。主要研究方向:计算流体力学。Tel.:010-82317019 E-mail:yanchao@buaa.edu.cn;李亚超 男,博士研究生。主要研究方向:计算流体力学。E-mail:yachaoli@foxmail.com

    通讯作者:

    阎超,Tel.:010-82317019 E-mail:yanchao@buaa.edu.cn

  • 中图分类号: V221.3

Some influence factors in aerodynamic heat transfer numerical simulation of jet-interaction flow

  • 摘要: 工程上对喷流气动热进行近似计算时,常常对真实的全化学反应流近似处理,这时需要了解喷流气体和喷管外形的近似方法对计算结果的影响规律。采用数值试验对比分析的方法,探讨了近似计算的2个影响因素:其一是使用量热完全的空气喷流近似燃气喷流进行数值模拟时,喷管几何形状对热流分布的影响;其二是使用空气喷流近似燃气喷流进行数值模拟的方法,分析不同的喷流热力学参数匹配方法对喷流形态及热流分布的影响。通过对不同方法进行对比计算,揭示了各个方法对喷流干扰气动热计算的影响规律,可以用于指导工程分析。

     

  • [1] WATANABE S,TAKAKI R,YAMAMOTO Y.RCS gas-jet interaction in the hypersonic flight experiment,HYFLEX:AIAA-1997-0524[R].Reston:AIAA,1997.
    [2] 耿云飞,阎超.联合激波针-逆向喷流方法的新概念研究[J].空气动力学学报,2010,28(4): 436-440. GENG Y F,YAN C.Numerical investigation on drag and heat-transfer reduction using combined spike and forward facing jet method[J].Acta Aerodynamica Sinica,2010,28(4):436-440(in Chinese).
    [3] GRAHAM M J,WEINACHT P,BRANDEIS J.Numerical investigation of supersonic jet interaction for finned bodies[J].Journal of Spacecraft and Rockets,2002,39(3):376-383.
    [4] 陈坚强,赫新,张毅锋,等.跨大气层飞行器RCS干扰数值模拟研究[J].空气动力学学报,2006,24(2):182-186. CHEN J Q,HE X,ZHANG Y F,et al.The numerical study on RCS interaction for trans-atmospheric vehicle[J].Acta Aerodynamica Sinica,2006,24(2):182-186(in Chinese).
    [5] 周松柏.超声速内外流干扰的数值方法研究及其实验验证与应用[D].长沙:国防科技大学,2009:28-33. ZHOU S B.Research on numerical method,experimental verification and application in simulation jet interaction in supersonic external flow[D].Changsha:National University of Defense Technology,2009:28-33(in Chinese).
    [6] 梁杰,阎超,李志辉,等.稀薄过渡流区横向喷流干扰效应数值模拟研究[J].空气动力学学报,2013,31(1):27-33. LIANG J,YAN C,LI Z H,et al.Numerical investigation of lateral jet interaction effects in rare field transition flow regime[J].Acta Aerodynamica Sinica,2013,31(1):27-33(in Chinese).
    [7] 邓有奇,阎超,吴晓军,等.战术导弹横向喷流数值模拟[J].北京航空航天大学学报,2005,31(4):477-480. DENG Y Q,YAN C,WU X J,et al.Numerical investigation of supersonic jet interactions for tactical bodies[J].Journal of Beijing University of Aeronautics and Astronautics,2005,31(4):477-480(in Chinese).
    [8] 杨彦广,刘君,唐志共.横向喷流干扰中的真实气体效应研究[J].空气动力学学报,2006,24(1):28-33. YANG Y G,LIU J,TANG Z G.A study of real gas effects on lateral jet interaction[J].Acta Aerodynamica Sinica,2006,24(1):28-33(in Chinese).
    [9] 李海燕,董维中,朱国林.高超声速喷管非平衡黏性流动的数值研究[J].航空学报,2006,27(2):204-207. LI H Y,DONG W Z,ZHU G L.Numerical simulation of non-equilibrium viscous flows in hypersonic nozzles[J].Acta Aeronautica et Astronautica Sinica,2006,27(2):204-207(in Chinese).
    [10] 贺旭照,秦思,曾学军,等.模拟飞行条件下的吸气式高超声速飞行器后体尾喷流干扰问题实验方案研究[J].推进技术,2014,35(10):1310-1316. HE X Z,QIN S,ZENG X J,et al.Experiment scheme research on afterbody nozzle plume interferenece of air-breathing hypersonic vehicle fly condition[J].Journal of Propulsion Technology,2014,35(10):1310-1316(in Chinese).
    [11] PINDZOLA M.Jet simulation in ground test facilities:AD-1963-440903[R].North Atlantic:AD,1963:11-13.
    [12] 李素偱.喷流控制飞行器姿态的物理问题[M].北京:中国宇航出版社,2003:93-94. LI S X.Physical problem of control aerocraft by jet[M].Beijing:China Astronautic Publishing House,2003:93-94(in Chinese).
    [13] CHAMBERLAIN R,DANG A A,MCCLURE D.Effect of exhaust chemistry on reaction jet control:AIAA-1999-0806[R].Reston:AIAA,1999.
    [14] PAO S P,DEERE K A,ABDOL-HAMID K S.Establishing approaches to modeling the ares I-X and ares I roll control system with free-stream interaction:AIAA-2011-1056[R].Reston:AIAA,2011.
    [15] 孙得川,杨建文,白荣博.喷流气体性质对导弹侧向喷流流场的影响[J].空气动力学学报,2010,28(6):720-723. SUN D C,YANG J W,BAI R B.The effect of gas properties on the lateral jet interaction flowfield[J].Acta Aerodynamica Sinica,2010,28(6):720-723(in Chinese).
    [16] HIRSCHEL E H,WEILAND C.高超声速飞行器启动热力学设计问题精选[M].唐志共,等,译.北京:国防工业出版社,2013:33-38. HIRSCHEL E H,WEILAND C.Selected aerothermodynamic design problems of hypersonic flight vehicles[M].TANG Z G,et al,translated.Beijing:National Defense Industry Press,2013:33-38(in Chinese).
    [17] 阎超.计算流体力学方法及应用[M].北京:北京航空航天大学出版社,2006:83-105. YAN C.Computational fluid dynamics theory and application[M].Beijing:Beihang University Press,2006:83-105(in Chinese).
    [18] GENG Y F,YU J,KONG W X.Investigation on a new method of adaptive drag reduction and non-ablation thermal protection system for hypersonic vehicles[J].Acta Aerodynamica Sinica,2012,30(4):492-501.
    [19] HAYASHI K,ASO S,TANI Y.Experimental study on thermal protection system by opposing jet in supersonic flow[J].Journal of Spacecraft & Rockets,2012,43(1):233-236.
  • 加载中
计量
  • 文章访问数:  909
  • HTML全文浏览量:  182
  • PDF下载量:  832
  • 被引次数: 0
出版历程
  • 收稿日期:  2015-06-09
  • 网络出版日期:  2016-06-20

目录

    /

    返回文章
    返回
    常见问答