Shock oscillation in highly underexpanded jets*

Project supported by the National Natural Science Foundation of China (Grant No. 11602028) and the Science and Technology Project of General Administration of Quality Supervision Inspection and Quarantine of China (Grant Nos. 2017QK119 and 2017QK188).

Li Xiao-Peng1, †, Zhou Rui2, Chen Xiao-Ping3, Fan Xue-Jun4, Xie Guo-Shan1
       

(color online) Comparison of shock screech amplitude obtained under different simulation conditions for NPR = 5.60: (a) amplitude of shock screech frequency f2s, (b) non-dimensional amplitude ratio of shock screech tone f2s.