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爆震波与涡轮叶片相互作用的数值模拟
引用本文:蒋联友,严传俊,邓君香,郑龙席.爆震波与涡轮叶片相互作用的数值模拟[J].航空动力学报,2009,24(1):60-64.
作者姓名:蒋联友  严传俊  邓君香  郑龙席
作者单位:西北工业大学,动力与能源学院,西安,710072
摘    要:应用计算流体力学(CFD)方法,对脉冲爆震波与涡轮叶片相互作用进行了初步数值模拟.以化学恰当比氢气空气混合物为反应物,仅考虑爆震波对涡轮静止叶片的作用.模拟结果表明:爆震波在通过涡轮叶片后,峰值压力发生衰减,并产生一向上游传播的激波,这有利于缓解爆震波对叶片的脉动冲击作用,但同时在涡轮叶片前缘会产生高压区,使叶片承受的应力很大.在爆震管出口压力变化图中可以看到由于激波经过叶片前缘和爆震室前端壁不断反射形成的多对不断衰减的双波峰.

关 键 词:脉冲爆震发动机  数值模拟  涡轮叶片  双波峰
收稿时间:12/7/2007 6:17:42 PM
修稿时间:2008/6/30 0:00:00

Numerical simulation of detonation wave interacting with turbine blade
JIANG Lian-you,YAN Chuan-jun,DENG Jun-xiang and ZHENG Long-xi.Numerical simulation of detonation wave interacting with turbine blade[J].Journal of Aerospace Power,2009,24(1):60-64.
Authors:JIANG Lian-you  YAN Chuan-jun  DENG Jun-xiang and ZHENG Long-xi
Institution:School of Power and Energy;Northwestern Polytechnical University;Xi'an 710072;China
Abstract:This paper conducted preliminary numerical simulation of their interactions by means of CFD method.The stoichiometric hydrogen-air mixture was employed as reactants and 1-step finite rate reaction model was used to investigate the interaction of detonation wave with a stationary blade.The simulation results indicate that the detonation wave attenuates after passing the blade passage,and generates a strong compression wave reflecting back upstream from leading edge of blade at the same time,This mitigates th...
Keywords:Pulse Detonation Engine  Numerical Simulation  Turbine Blade
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