Compressible starting jet: pinch-off and vortex ring-trailing jet interaction

被引:35
作者
Fernandez, Juan Jose Pena [1 ]
Sesterhenn, Jorn [1 ]
机构
[1] Tech Univ Berlin, Inst Stromungsmech & Tech Akust, D-10623 Berlin, Germany
关键词
compressible flows; jets; jet noise; DIRECT NUMERICAL-SIMULATION; SHOCK ASSOCIATED NOISE; SUPERSONIC JETS; TURBULENT JET; MIXING NOISE; SOUND FIELD; LAMINAR; CIRCULATION; VELOCITY; NOZZLES;
D O I
10.1017/jfm.2017.128
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The dominant feature of the compressible starting jet is the interaction between the emerging vortex ring and the trailing jet. There are two types of interaction: the shock-shear layer-vortex interaction and the shear layer-vortex interaction. The former is clearly not present in the incompressible case, since there are no shocks. The shear layer-vortex interaction has been reported in the literature in the incompressible case and it was found that compressibility reduces the critical Reynolds number for the interaction. Four governing parameters describe the compressible starting jet: the non-dimensional mass supply, the Reynolds number, the reservoir to unbounded chamber temperature ratio and the reservoir to unbounded chamber pressure ratio. The latter parameter does not exist in the incompressible case. For large Reynolds numbers, the vortex pinch-off takes place in a multiple way. We studied the compressible starting jet numerically and found that the interaction strongly links the vortex ring and the trailing jet. The shear layer-vortex interaction leads to a rapid breakdown of the head vortex ring when the flow impacted by the Kelvin-Helmholtz instabilities is ingested into the head vortex ring. The shock-shear layer-vortex interaction is similar to the noise generation mechanism of broadband shock noise in a continuously blowing jet and results in similar sound pressure amplitudes in the far field.
引用
收藏
页码:560 / 589
页数:30
相关论文
共 55 条
[1]   A high-resolution hybrid compact-ENO scheme for shock-turbulence interaction problems [J].
Adams, NA ;
Shariff, K .
JOURNAL OF COMPUTATIONAL PHYSICS, 1996, 127 (01) :27-51
[2]  
Anderson Dale, 2020, Computational Fluid Mechanics and Heat Transfer
[3]  
[Anonymous], THESIS
[4]  
[Anonymous], SAND808617
[5]  
[Anonymous], 1867, PHILOS MAG, V33, P511
[6]   Direct numerical simulation of vortex ring evolution from the laminar to the early turbulent regime [J].
Archer, P. J. ;
Thomas, T. G. ;
Coleman, G. N. .
JOURNAL OF FLUID MECHANICS, 2008, 598 (201-226) :201-226
[7]   The flow field in turbulent round free jets [J].
Ball, C. G. ;
Fellouah, H. ;
Pollard, A. .
PROGRESS IN AEROSPACE SCIENCES, 2012, 50 :1-26
[8]  
Becker E., 1968, Gas Dynamics
[9]   A shock-capturing methodology based on adaptative spatial filtering for high-order non-linear computations [J].
Bogey, Christophe ;
de Cacqueray, Nicolas ;
Bailly, Christophe .
JOURNAL OF COMPUTATIONAL PHYSICS, 2009, 228 (05) :1447-1465
[10]   VELOCITY-FIELD OF AN AXISYMMETRICAL PULSED, SUBSONIC AIR-JET [J].
BREMHORST, K ;
HOLLIS, PG .
AIAA JOURNAL, 1990, 28 (12) :2043-2049