Sidewall influence of varying free stream Mach number in ramp induced shock wave boundary layer interactions  

作　　者：Raja Mangalagiri Satya P.Jammy 

机构地区：[1]Department of Mechanical Engineering,SRM University AP,Andhra Pradesh 522502,India

出　　处：《Theoretical & Applied Mechanics Letters》2024年第4期298-305,共8页力学快报（英文版）

基　　金：sponsored by the Department of Science and Technology,Science and Engineering Research Board(SERB),Core Research(Grant No.CRG/2020/03859)。

摘　　要：This study investigates the three-dimensional(3D)effects introduced by the end walls for an aspect ratio of1 in ramp-induced shock wave boundary layer interactions.The simulations are performed using a symmetry boundary condition in the spanwise direction at free-stream Mach numbers in 3D.The simulations are performed using an in-house compressible supersonic solver“Open SBLIFVM”.Two free stream Mach numbers 2.5,and3 are used in the current work,and the simulated results are compared with the aspect ratio 1 simulations by Mangalagiri and Jammy.The inflow is initialized with a similarity solution;its Reynolds number based on the boundary layer thickness is adjusted such that the Reynolds number at the start of the ramp is kept at 3×10^(5)for all simulations.From the results,it is evident that the introduction of sidewalls resulted in a shorter centerline separation length when compared with the two-dimensional(2D)simulations.This contradicts the results at Mach 2 by Mangalgiri and Jammy where the vortex observed at Mach 2 in the central separation region disappeared with increasing free-stream Mach number.Additionally,the topology of interaction shifted from owl-like separation of the second kind to the first kind when the freestream Mach number increased from2 to 2.5.It can be concluded that the interaction topology is crucial to the increase or decrease of the central separation length when compared to 2D simulations.

关 键 词：Shock boundary layer interaction Separation Compressible boundary layers GPGPU simulations RSWBLI 

分 类 号：U461[机械工程—车辆工程]