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二元收-扩喷管气动喉道控制数值模拟

郭飞飞 王如根 吴培根

郭飞飞, 王如根, 吴培根. 二元收-扩喷管气动喉道控制数值模拟[J]. 航空动力学报, 2014, (10): 2303-2310. doi: 10.13224/j.cnki.jasp.2014.10.005
引用本文: 郭飞飞, 王如根, 吴培根. 二元收-扩喷管气动喉道控制数值模拟[J]. 航空动力学报, 2014, (10): 2303-2310. doi: 10.13224/j.cnki.jasp.2014.10.005
GUO Fei-fei, WANG Ru-gen, WU Pei-gen. Numerical simulation of two-dimensional convergent-divergent nozzle with pneumatic throat control[J]. Journal of Aerospace Power, 2014, (10): 2303-2310. doi: 10.13224/j.cnki.jasp.2014.10.005
Citation: GUO Fei-fei, WANG Ru-gen, WU Pei-gen. Numerical simulation of two-dimensional convergent-divergent nozzle with pneumatic throat control[J]. Journal of Aerospace Power, 2014, (10): 2303-2310. doi: 10.13224/j.cnki.jasp.2014.10.005

二元收-扩喷管气动喉道控制数值模拟

doi: 10.13224/j.cnki.jasp.2014.10.005
详细信息
    作者简介:

    郭飞飞(1984- ),男,陕西宝鸡人,博士生,主要从事航空发动机气动热力理论与工程的研究.

  • 中图分类号: V231

Numerical simulation of two-dimensional convergent-divergent nozzle with pneumatic throat control

  • 摘要: 设计了收敛段为圆转方段的二元收-扩喷管,对喉道面积气动射流控制方案进行了数值模拟,分析了喷管出口宽高比、落压比、射流角度对喉道面积和喷管性能的影响.结果表明:喷管喉道矩形截面宽边壁面附近的静压小于窄边壁面附近的静压,并且随着出口宽高比的增大,宽边壁面附近的静压逐渐减小,窄边壁面附近的静压逐渐增大;在同样的落压比下,出口宽高比增大,喉道面积控制范围(RTAC)、喉道面积控制效率(ETAC)增大,总压恢复系数减小;出口宽高比一定时,随落压比的增大,RTAC,ETAC先减小而后基本保持不变,总压恢复系数增大;ETAC随射流角度的增大而增大.

     

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出版历程
  • 收稿日期:  2013-06-21
  • 刊出日期:  2014-10-28

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