Computational study of supersonic flow past non-stationary obstructions part-II - moving protrusion

被引:0
|
作者
Deshpande, Vikram [1 ]
Eshpuniyani, Brijesh [2 ]
Sanghi, Sanjeev [1 ]
机构
[1] Indian Inst Technol Delhi, Dept Appl Mech, New Delhi 110016, India
[2] Indian Inst Technol BHU, Dept Mech Engn, Varanasi 221005, Uttar Pradesh, India
来源
PROGRESS IN COMPUTATIONAL FLUID DYNAMICS | 2015年 / 15卷 / 03期
关键词
supersonic flow; moving protrusion; shock wave boundary layer interaction; SWBLI; pressure hysteresis; particle velocity upwinding scheme; PVUS;
D O I
10.1504/PCFD.2015.069579
中图分类号
O414.1 [热力学];
学科分类号
摘要
For an upward moving protrusion, recirculation regions develop on both sides with separation/reattachment distances increasing with protrusion height while being smaller than the corresponding fixed protrusion values. Differences in upstream wall pressures between moving versus fixed protrusions are reasoned in terms of: 1) extent of coalescence of upstream travelling compression waves into a shock; 2) inclination of this shock wave with free stream; 3) a low velocity high pressure band of fluid formed adjacent to the protrusion fore surface. Downstream wall pressures are lower than the corresponding fixed protrusion values due to a higher expansion of the flow for the range of protrusion heights considered. For an oscillating protrusion, wall pressure response to varying protrusion heights displays a hysteretic behaviour. Compressive/expansive effects generated during the protrusion's upward/downward motions persist alter the protrusion changes its direction. Higher upstream and lower downstream wall pressures are observed in general at higher protrusion velocities.
引用
收藏
页码:157 / 167
页数:11
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