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

变循环发动机模态转换数值模拟

刘增文 王占学 蔡元虎

刘增文, 王占学, 蔡元虎. 变循环发动机模态转换数值模拟[J]. 航空动力学报, 2011, 26(9): 2128-2132.
引用本文: 刘增文, 王占学, 蔡元虎. 变循环发动机模态转换数值模拟[J]. 航空动力学报, 2011, 26(9): 2128-2132.
LIU Zeng-wen, WANG Zhan-xue, CAI Yuan-hu. Numerical simulation on bypass transition of variable cycle engines[J]. Journal of Aerospace Power, 2011, 26(9): 2128-2132.
Citation: LIU Zeng-wen, WANG Zhan-xue, CAI Yuan-hu. Numerical simulation on bypass transition of variable cycle engines[J]. Journal of Aerospace Power, 2011, 26(9): 2128-2132.

变循环发动机模态转换数值模拟

Numerical simulation on bypass transition of variable cycle engines

  • 摘要: 对双外涵变循环发动机的模态转换过程进行了研究,设计了变循环发动机模态转换方案,确立了模态转换时的多部件调节规律,采用稳态模型对模态转换进行了数值模拟.结果表明,所设计的模态转换方案可行,能够使变循环发动机的涵道比发生明显改变,并有效提高了发动机在部分推力时的空气流量,与设计参数相同的常规涡扇发动机相比,其安装耗油率明显降低.

     

  • [1] Johnson J E.Variable cycle engines-the next step in propulsion evolution .AIAA 1976-758,1976.
    [2] Sherwood H.Bibliography of supersonic cruise research (SCR) program from 1977 to mid-1980 .NASA RP 1063,1980.
    [3] Allan R D.Advanced supersonic propulsion system technology study .NASA CR-134913,1975.
    [4] Howlett R A,Sabatella J,Johnson J,et al.Advanced supersonic propulsion study .NASA CR-134904,1975.
    [5] Allan R D.General electric company variable cycle engine technology demonstrator program .AIAA 1979-1311,1979.
    [6] Bratley R.Versatile affordable advanced turbine engines (VAATE BAA Ⅲ) .BAA-07-01-PRK,2007.
    [7] Nascimento M A.The selective bleed variable cycle engine .Cranfield:Cranfield University,1992.
    [8] Habrard A.The variable-cycle engine a solution to the economical and environmental challenge of the future supersonic transport //Symposium on Future Supersonic and Hypersonic Transportation System.France:Strasbourg,1989:211-218.
    [9] Miyagi H,Kimura H,Kishi K,et al. Combined cycle engine research in Japanese HYPR program .AIAA 1998-3278,1998.
    [10] James E.Turbofan engine with a core driven supercharged bypass duct and fixed geometry nozzle:US,5806303 .1998-09-15.
    [11] Giffin R G,Johnson J E,Crall D W,et al.Turbofan engine with a core driven supercharged bypass duct:US,5809772 .1998-09-22.
    [12] Shelby J M,Jr,Walter P N,Jr,Rodney O B.A simplified analysis of propulsion installation losses for computerized aircraft design .NASA TM X-73136,1976.
  • 加载中
计量
  • 文章访问数:  2364
  • HTML浏览量:  330
  • PDF量:  37
  • 被引次数: 0
出版历程
  • 收稿日期:  2010-09-12
  • 修回日期:  2011-03-29
  • 刊出日期:  2011-09-28

目录

    /

    返回文章
    返回