Oscillatory modes of interaction of supersonic overexpanded jets with barriers |
| |
Authors: | O V Bocharova M G Lebedev |
| |
Institution: | 1.Faculty of Computational Mathematics and Cybernetics,Moscow State University,Moscow,Russia |
| |
Abstract: | The self-oscillatory interaction of supersonic jets with barriers has mainly been studied for under-expanded jets. There are
only a few experimental studies examining the case of overexpanded jets, with little computational work done in this direction.
To fill this gap, we performed numerical simulations of overexpanded supersonic jets with barriers. The calculations were
performed by the Godunov method on fine grids using parallel programming techniques. In the course of numerical simulations,
the gasdynamic parameters of the jet and the geometric parameter of the barrier were varied. The barrier had the shape of
a cylindrical cavity of depth l = (0 − 18)r
a
, where r
a
is the nozzle exit radius (the case l = 0 corresponds to a flat-end barrier). Based on the results of the numerical simulations, the conclusion on whether the
self-oscillation process occurs was drawn and the dependence its characteristics (frequency and amplitude) on the governing
gasdynamic and geometric parameters were obtained. Good agreement with experimental data on the fundamental tone frequency
was demonstrated. A low-frequency oscillation mode was mostly realized. In this case, the jet experienced periodic suctions
into and ejections from the cavity, counter the oncoming jet flow, with the formation of a structure consisting of three discontinuity
surfaces (two shock waves and a separating surface contact). |
| |
Keywords: | |
本文献已被 SpringerLink 等数据库收录! |
|