Investigation and quantification of flow unsteadiness in shock-particle cloud interaction

被引:36
作者
Hosseinzadeh-Nik, Zahra [1 ,2 ]
Subramaniam, Shankar [2 ]
Regele, Jonathan D. [1 ]
机构
[1] Iowa State Univ, Dept Aerosp Engn, Ames, IA 50010 USA
[2] Iowa State Univ, Dept Mech Engn, Ctr Multiphase Flow Res & Educ CoMFRE, Ames, IA 50010 USA
关键词
Shock-particle interaction; Unsteadiness; Vorticity equation; Velocity fluctuations; WAVELET-COLLOCATION METHOD; COMPRESSIBLE VISCOUS FLOWS; NUMERICAL-SIMULATION; EVOLUTION PROBLEMS; DUSTY-GAS; DYNAMICS; CYLINDER; DIFFRACTION; COMPUTATION; SPHERES;
D O I
10.1016/j.ijmultiphaseflow.2018.01.011
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This work aims to study the interaction of a shock wave with a cloud of particles to quantify flow unsteadiness and velocity fluctuations using particle-resolved direct numerical simulation (PR-DNS). Three cases are studied, with each case revealing one aspect of the intricate flow phenomena involved in this interaction. The unsteady interaction of a shock wave with a transverse array of particles reveals the origin of unsteadiness under the effect of mutual wave-wave and wave-wake interactions between the particles. In the second case, the interaction of a shock with a particle cloud is studied, with a focus on the interaction of the complex wave system with the vortical structure. A budget analysis of the vorticity equation reveals the sources of strong unsteadiness in the particle cloud. A detailed analysis of the velocity fluctuation and kinetic energy in the fluctuating motion is performed to ascertain the importance of the velocity fluctuations that arise from the strong unsteadiness. An analogous analysis is presented, in the third case, for a gradually-induced flow on the same particle cloud along with a comparison to the shock induced case to assess the impulsive effect of shock on intensity of the fluctuating field statistics. (C) 2018 Elsevier Ltd. All rights reserved.
引用
收藏
页码:186 / 201
页数:16
相关论文
共 60 条
[1]  
Abe A, 2001, COMPUTAT ENGN, V3, P209
[2]  
[Anonymous], 1988, 269 UTIAS
[3]   A 2-PHASE MIXTURE THEORY FOR THE DEFLAGRATION-TO-DETONATION TRANSITION (DDT) IN REACTIVE ANTIGRANULOCYTES-MATERIALS [J].
BAER, MR ;
NUNZIATO, JW .
INTERNATIONAL JOURNAL OF MULTIPHASE FLOW, 1986, 12 (06) :861-889
[4]  
Bhagatwala A. V., 2011, THESIS
[5]  
Bredin M, 2007, R D J S AFR I MECH E
[6]   A characteristic based volume penalization method for general evolution problems applied to compressible viscous flows [J].
Brown-Dymkoski, Eric ;
Kasimov, Nurlybek ;
Vasilyev, Oleg V. .
JOURNAL OF COMPUTATIONAL PHYSICS, 2014, 262 :344-357
[7]  
Bryson A. E, 1960, FLUID MECH, V10, P1
[8]   On the use of immersed boundary methods for shock/obstacle interactions [J].
Chaudhuri, Arnab ;
Hadjadj, Abdellah ;
Chinnayya, Ashwin .
JOURNAL OF COMPUTATIONAL PHYSICS, 2011, 230 (05) :1731-1748
[9]   Numerical investigation of the compressible flow past an aerofoil [J].
Chen, Li-Wei ;
Xu, Chang-Yue ;
Lu, Xi-Yun .
JOURNAL OF FLUID MECHANICS, 2010, 643 :97-126
[10]   Characteristic development of hyperbolic two-dimensional two-fluid model for gas-liquid flows with surface tension [J].
Chung, Moon-Sun .
APPLIED MATHEMATICAL MODELLING, 2007, 31 (03) :578-588