The influence of radial entrance width of the circular cavity on incident shock wave focusing  

作　　者：Xin Chen Chuan Wang Sheng Tan Liming He Qiang Zhang 

机构地区：[1]Aeronautics and Astronautics Engineering College,Air Force Engineering University,Xi’an 710038,China [2]Aerospace Science and Engineering College,National University of Defense Technology,Changsha 410071,China

出　　处：《Propulsion and Power Research》2018年第2期120-128,共9页推进与动力（英文）

基　　金：the National Natural Science Foundation of China under Grant no.51106178.

摘　　要：Despite the achievement of shock wave focusing with certain reflectors,the influence of the radial entrance width of a circular cavity on the flow field has yet to be addressed.In this study,we systematically investigated the effects of the shock wave focusing process in a cavity based on the radial entrance widths.An experimental system was installed to research the evolution of the flow field under conditions with different radial entrance widths of 3.0,11.1,19.5,and 33.0 mm.A schlieren system was used to photograph the structures of the flow field in the cavity,and a data acquisition system was used to record the dynamic pressure histories of different points.A numerical simulation was carried out to investigate greater details of the shock wave focusing process.A third-order strong stability-preserving Runge-Kutta method,third-order weighed essential non-oscillation scheme,and an adaptive mesh refinement algorithm were adopted to simulate the shock wave reflection,diffraction,and focus process.Good agreement between the experimental and numerical results was observed.By comparing the evolution process of the flow field under the conditions of four different entrance cavity widths,we found that when the entrance width was 19.5 mm,there was the stronger intensity of the shock wave focusing in the focal region,and the larger pressure value at the apex of the cavity than the other three entrance widths,occur.This study improves our understanding of shock wave focusing.

关 键 词：Shock wave focusing Radial entrance widths Cavity Schlieren system Weighed essential nonoscillation 

分 类 号：O35[理学—流体力学]