Quasi-steady aerodynamic characteristics of Terminal Sensitive Bullets with short cylindrical portion  

作　　者：Yong-liang Yang Rui Guo Rong-zhong Liu Liang Chen Bo-yang Xing Bo-bo Zhao 

机构地区：[1]School of Mechanical Engineering,Nanjing University of Science and Technology,Xiaolingwei 200,210094,Nanjing,China [2]The Seventh Design Department,Aerospace Science and Technology Corporation,The Seventh Research Institute,610100,Chengdu,China [3]Unit 31102 of PLA,210000,Nanjing,China

出　　处：《Defence Technology（防务技术）》2021年第2期633-649,共17页Defence Technology

基　　金：The authors would like to acknowledge the financial supports from the National Natural Science Foundation of China(Grant No.11372136);the Special fund for basic scientific research of Central University(Grant No.30916011306);the Postgraduate Research&Practice Innovation Program of Jiangsu Province(Grant No.KYCX17_0386).

摘　　要：The aerodynamic characteristics are vital for short cylindrical Terminal Sensitive Bullets(TSB)with lowaspect ratio,especially in terminal trajectory.Currently,there is little research in terms of the TSB andshort cylinder with two free ends,and particularly in this trajectory,where the scanning angleβand rollangle a vary over a broad range between 0°and 180.In this work wind tunnel experiments are firstconducted to learn the effects of Reynolds number and scanning angle on aerodynamic parameters forshort cylinder with aspect ratio L/D=1.Similar to infinite cylinder,for the short cylinder with two freeends,the drag crisis phenomenon still exists in the critical regime 1.7×10^(5)≤Re≤6.8×10^(5).Then 3Dsimulations are performed to demonstrate the aerodynamic characteristics of short cylinder and TSBover a broad range of Re,L/D,a and 6.The sensitivity analysis of time step and grid are presented as well.whenβ3=0,for short cylinder,the drag crisis phenomenon was also observed in the simulation,but notas obvious as in the wind tunnel test.In some attitudes,there is an obvious Karman vortexin the wake ofshort cylinder and TSB.The correlation between time-averaged aerodynamic coefficients and L/D,Re,a&l is discussed.The vortex shedding frequency and shear layer behavior are obtained for quasi-steadyand unsteady flow.Finally,the effect of end's shape on drag reduction and vortex shedding frequency isanalyzed.

关 键 词：Turbulent flows around bluff body Critical regime Flow-induced structural vibration 

分 类 号：TJ410.1[兵器科学与技术—火炮、自动武器与弹药工程]