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轴向长度对旋转爆震发动机的影响

陈洁 王栋 马虎 刁吉阳 于栋梁

陈洁, 王栋, 马虎, 刁吉阳, 于栋梁. 轴向长度对旋转爆震发动机的影响[J]. 航空动力学报, 2013, 28(4): 844-849.
引用本文: 陈洁, 王栋, 马虎, 刁吉阳, 于栋梁. 轴向长度对旋转爆震发动机的影响[J]. 航空动力学报, 2013, 28(4): 844-849.
CHEN Jie, WANG Dong, MA Hu, DIAO Ji-yang, YU Dong-liang. Influence of axial length on rotating detonation engine[J]. Journal of Aerospace Power, 2013, 28(4): 844-849.
Citation: CHEN Jie, WANG Dong, MA Hu, DIAO Ji-yang, YU Dong-liang. Influence of axial length on rotating detonation engine[J]. Journal of Aerospace Power, 2013, 28(4): 844-849.

轴向长度对旋转爆震发动机的影响

Influence of axial length on rotating detonation engine

  • 摘要: 采用9组分19步基元反应模型,不考虑黏性、热传导和扩散效应等对流动的影响,对以氢气和氧气为反应混合物的旋转爆震发动机内流场进行计算,研究轴向长度对发动机性能的影响.研究表明:在一定范围内轴向长度对发动机比冲影响很小,轴向长度过长时会降低发动机比冲.轴向长度对爆震波的压力形成影响很大,轴向长度过小时,爆震波压力不高,过大时,会导致斜激波压力衰减.随着轴向长度的增加,由于膨胀的作用,出口的压 力不断降低,轴向长度为200mm时,出口的平均速度最大,此时发动机比冲也达到最大值;周向速度明显减小,降低了周向速度对发动机的不利影响;推力密度峰值逐渐下降;激波前后密度差逐渐减小,这使发动机的推力偏心矩也不断降低,从而可有效地减小角散布等不利影响.

     

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出版历程
  • 收稿日期:  2012-05-15
  • 刊出日期:  2013-04-28

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