1 / 2020-07-30 19:25:12
Investigation on Design Method of Curved Compression Surface
Inlet; Curved compression surface; Design method; Numerical simulation
全文待审
Pan Jin / Jiangsu Maritime Institute
Suppose that curved compression surface consists of segments. Two curved surfaces formed by equal compression angles of the micro-element segments and a slight increase in the compression angle of the micro-element segments are designed respectively. The numerical simulation method is used to compare the performance of two curved surfaces with the reference three-wedge compression surface. Select NASA classic test data, in order to determine the turbulence model and calculation method chosen by the numerical simulation Fluent software. The results show: the configuration of the segment compression angle deeply affects compression efficiency of the curved surface compression system. Pressure gradient distribution on the compression surface with constant compression angles segments is nearly constant along the incoming flow direction, and the curved compression surface easily resist the separation of the boundary layer compared to three-wedges compression surface. The approximate calculation method of the bending shock profile is given.
重要日期
  • 会议日期

    10月30日

    2020

    11月01日

    2020

  • 08月30日 2020

    初稿截稿日期

  • 11月01日 2020

    注册截止日期

主办单位
中国力学学会流体控制工程专业委员会
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重庆理工大学
哈尔滨工业大学
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日本流体动力系统学会
燕山大学
中国民航大学
吉林大学
昆明理工大学国际技术转移中心
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