首页|双钟形喷管流动振荡特性的实验研究

双钟形喷管流动振荡特性的实验研究

Experimental study on flow oscillation characteristics of dual-bell nozzles

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为揭示双钟形喷管内的流动振荡现象,开展了不同延伸段压力分布的双钟形喷管流动振荡特性的风洞实验研究,获得了不同流动状态下的流场振荡特性.结果表明,不论处于分离还是满流状态下,双钟形喷管流场均存在由回流区声学谐振和激波非定常脉动引起的低频振荡(约 180 Hz)现象.然而,在分离不断增大的过程中,激波脉动被抑制,振荡现象显著减弱.当快速模态逆转换过程完成后,在分离激波由运动突然转为相对稳定时,流动产生一定的冲击效应,振荡幅值被放大约 5 倍,随后又迅速衰减.在双钟形喷管的结构设计过程中,需要避免喷管结构的特征频率与流动振荡的特征频率共振,同时需关注快速模态转换完成后的冲击载荷.
To understand the phenomenon of flow oscillation in the dual-bell nozzle,a wind tunnel test was conducted to study the flow oscillation characteristics of dual-bell nozzles with different extension pressure distributions.Flow field oscillation character-istics under different flow states were obtained.The results show that,there are low-frequency fluctuation about 180 Hz caused by the acoustic resonance in the recirculation zone and the unsteady pulsation of shock wave in the flow field of dual-bell nozzles under both the separation state and the full-flow state.However,when the separation gradually increase,the shock system pulsation is sup-pressed and the oscillation phenomenon is significantly weakened.Specifically,when the separation shock suddenly changes from mo-tion to relatively static after the fast mode re-transition,the flow produces an impact effect,and the oscillation amplitude is amplified about 5 times,but then rapidly attenuated.In engineering practice,the structural design of dual-bell nozzles should ensure the char-acteristic frequency of the nozzle structure away from the characteristic frequency of flow oscillation to avoid resonance.Meanwhile,the impact load after fast mode transition should also be taken into consideration in the design of dual-bell nozzle structures.

dual-bell nozzleflow separationlow frequency oscillationshock wave pulsation

刘亚洲、王壮、胡海峰、杨建文

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西安航天动力研究所,西安 710100

双钟形喷管 流动分离 低频振荡 激波脉动

2024

固体火箭技术
中国航天科技集团公司第四研究院 中国宇航学会固体推进专业委员会

固体火箭技术

CSTPCD北大核心
影响因子:0.461
ISSN:1006-2793
年,卷(期):2024.47(6)