SPATIAL STRUCTURE OF A CONFINED SWIRLING FLOW USING PLANAR ELASTIC SCATTER IMAGING AND LASER-DOPPLER VELOCIMETRY

被引:6
|
作者
EDWARDS, CF
FORNACIARI, NR
DUNSKY, CM
MARX, KD
ASHURST, WT
机构
[1] Combustion Research Facility, Sandia National Laboratories, Livermore
关键词
COMBUSTION FURNACE; FLAME; KINETICS;
D O I
10.1016/0016-2361(93)90324-U
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
This paper reports the results of a study of the instantaneous spatial structure of a confined swirling flow after a sudden expansion. The flow chosen corresponds to the cold flow conditions of an axisymmetric laboratory-scale research furnace. The swirl number of the flow is 0.7 at the inlet plane and the expansion diameter ratio is 6:1. The flow has a centre hub-to-throat diameter ratio of 1:4. Data are reported for the instantaneous spatial structure of the flow via transient planar elastic scattering imaging. This technique allows for unambiguous visualization of the spatial structure of the flow by slicing through it with a thin sheet (approximately 1.5 mm) of light at various locations in the axial/radial and radial/azimuthal planes. By varying the time delay between introduction of the seeding material and data acquisition, features of the flow that would ordinarily be inaccessible are revealed. Laser Doppler velocimetry is used to measure the time-averaged and root mean square velocity components in all three coordinate directions. Using these data, we construct a model of the flow from the viewpoint of the vorticity fed into the flow and its subsequent dynamics. This viewpoint suggests different reasons for the development of the observable features of the flow and shows promise for helping to deconvolve the apparent complexity of this flowfield.
引用
收藏
页码:1151 / 1159
页数:9
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