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非对称喷管超声速流场的PIV实验与数值模拟

俞凯凯 徐惊雷 马静

俞凯凯, 徐惊雷, 马静. 非对称喷管超声速流场的PIV实验与数值模拟[J]. 航空动力学报, 2012, 27(9): 2041-2047.
引用本文: 俞凯凯, 徐惊雷, 马静. 非对称喷管超声速流场的PIV实验与数值模拟[J]. 航空动力学报, 2012, 27(9): 2041-2047.
YU Kai-kai, XU Jing-lei, MA Jing. PIV experimental study and numerical simulation of single expansion ramp nozzle supersonic flow field[J]. Journal of Aerospace Power, 2012, 27(9): 2041-2047.
Citation: YU Kai-kai, XU Jing-lei, MA Jing. PIV experimental study and numerical simulation of single expansion ramp nozzle supersonic flow field[J]. Journal of Aerospace Power, 2012, 27(9): 2041-2047.

非对称喷管超声速流场的PIV实验与数值模拟

基金项目: 国家自然科学基金(50876042,90916032)

PIV experimental study and numerical simulation of single expansion ramp nozzle supersonic flow field

  • 摘要: 选取了跟随性能以及散射性能都上佳的二氧化钛粒子,利用了粒子图像测速仪(particle image velocimetry,PIV)对不同落压比下的非对称喷管(single expansion ramp nozzle,SERN)流场进行了测量,成功获取了相应流动结构,以及沿程上壁面压力分布和速度场等.在测得的图像中,可以清晰地观察到由于过膨胀产生的激波与膨胀波系,并进一步获得出口速度分布.运用计算流体动力学数值模拟方法,对实验状态下的非对称喷管进行了模拟.对比结果发现:PIV实验测得流场结构能很好地与其吻合,这互相验证了CFD计算和PIV实验的正确性及可靠性.

     

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出版历程
  • 收稿日期:  2011-10-18
  • 刊出日期:  2012-09-28

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