Turbulent flame augmentation using a fluidic jet for Deflagration-to-Detonation

被引:39
作者
Chambers, Jessica [1 ]
Ahmed, Kareem [1 ]
机构
[1] Univ Cent Florida, Dept Mech & Aerosp Engn, Ctr Adv Turbomachinery & Energy Res, Prop & Energy Res Lab, Orlando, FL 32816 USA
关键词
Turbulent premixed combustion; Flame-turbulence interactions; Deflagration-to-Detonation; Flame structural dynamics; Methane flames; THERMODYNAMIC CYCLE ANALYSIS; PROPULSION APPLICATIONS; TRANSITION;
D O I
10.1016/j.fuel.2017.03.023
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
Detonation is a high energetic mode of pressure gain combustion that exploits total pressure rise to augment high flow momentum and thermodynamic efficiencies. Detonation is initiated through flame acceleration driven by turbulence interaction and induction for Deflagration-to-Detonation Transition (DDT). There is a broad desire to unravel the physical mechanisms of turbulence induced DDT. The study examines the role of turbulence induced by a fluidic jet on turbulent accelerating flames. The investigation aims to classify the turbulent flame dynamics and temporal evolution of the flame stages throughout the turbulent regimes. The flame-flow interactions are experimentally studied in a detonation facility using high-speed particle image velocimetry (PIV) and Schlieren imaging. The analysis explores the local turbulence and flame acceleration mechanisms that result from the high level of turbulent transport induced by the jet. Higher flame acceleration is observed for the turbulent flame relative to the laminar flame. The turbulent flame experiences high propagation of turbulence intensities in the lower flame boundary. An increase in vorticity generation, velocity fluctuation, and turbulent strain-rate is experienced throughout the interaction. The turbulent flame regime is characterized showing an evolution between the thin-to-broken reactions. (C) 2017 Elsevier Ltd. All rights reserved.
引用
收藏
页码:616 / 626
页数:11
相关论文
共 39 条
[1]  
[Anonymous], 2011, RANDOM DATA ANAL MEA
[2]   STUDIES OF TURBULENT FLOW-FLAME INTERACTION [J].
BALLAL, DR .
AIAA JOURNAL, 1986, 24 (07) :1148-1154
[3]  
Borghi R., 1985, RECENT ADV AEROSPACE, P117, DOI DOI 10.1007/978-1-4684-4298-4_7
[4]  
Bray K., 1995, P ROYAL SOC LOND MAT
[5]   Spatially correlated precision error in digital particle image velocimetry measurements of turbulent flows [J].
Carr, Z. R. ;
Ahmed, K. A. ;
Forliti, D. J. .
EXPERIMENTS IN FLUIDS, 2009, 47 (01) :95-106
[6]   Flame acceleration and transition to detonation in ducts [J].
Ciccarelli, G. ;
Dorofeev, S. .
PROGRESS IN ENERGY AND COMBUSTION SCIENCE, 2008, 34 (04) :499-550
[7]   Direct experimental impulse measurements for detonations and deflagrations [J].
Cooper, M ;
Jackson, S ;
Austin, J ;
Wintenberger, E ;
Shepherd, JE .
JOURNAL OF PROPULSION AND POWER, 2002, 18 (05) :1033-1041
[8]  
Damkohler G., 1940, Z ELEKTROCHEM, V46, P601
[9]  
Day M.S., 2006, P EUR C COMP FLUID D
[10]   REVIEW OF PROPULSION APPLICATIONS AND NUMERICAL SIMULATIONS OF THE PULSED DETONATION ENGINE CONCEPT [J].
EIDELMAN, S ;
GROSSMANN, W ;
LOTTATI, I .
JOURNAL OF PROPULSION AND POWER, 1991, 7 (06) :857-865