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基于侧向膨胀影响爆震波的自持机理

周朱林 刘卫东 刘世杰 林志勇

周朱林, 刘卫东, 刘世杰, 林志勇. 基于侧向膨胀影响爆震波的自持机理[J]. 航空动力学报, 2013, 28(9): 1967-1974.
引用本文: 周朱林, 刘卫东, 刘世杰, 林志勇. 基于侧向膨胀影响爆震波的自持机理[J]. 航空动力学报, 2013, 28(9): 1967-1974.
ZHOU Zhu-lin, LIU Wei-dong, LIU Shi-jie, LIN Zhi-yong. Self-sustaining mechanism of detonation wave influenced by lateral expansion[J]. Journal of Aerospace Power, 2013, 28(9): 1967-1974.
Citation: ZHOU Zhu-lin, LIU Wei-dong, LIU Shi-jie, LIN Zhi-yong. Self-sustaining mechanism of detonation wave influenced by lateral expansion[J]. Journal of Aerospace Power, 2013, 28(9): 1967-1974.

基于侧向膨胀影响爆震波的自持机理

基金项目: 国家自然科学基金(51006119,90816016)

Self-sustaining mechanism of detonation wave influenced by lateral expansion

  • 摘要: 为了研究受侧向膨胀影响时爆震波的传播特性及自持机理,在实验段对比分析了当量比(0.70~2.25)和波前预混气高度(1,2,3cm)对爆震波自持传播能力的影响.实验表明:波前预混气高度越高、预混气活性越强,则爆震波抵御侧向膨胀影响的能力越强,速度亏损越小,自持传播能力越强.运用Fay流体扩张理论,Dabora和Murray速度亏损理论,并结合Zeldovich-von Neumann-Döring(ZND)模型对受侧向膨胀影响的爆震波激波角、界面角和速度亏损进行理论预测,证明Dabora的理论预测与实验值吻合很好,且发现若要受侧向膨胀影响的爆震波自持传播,则其速度亏损的极限为7.0%~11.0%.

     

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出版历程
  • 收稿日期:  2012-09-21
  • 刊出日期:  2013-09-28

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