The main objective of this study is to clarify effects of flame straining on flame structures and heat release rate (HRR) of swirling flames. This is achieved by analyzing results of direct numerical simulations (DNS) of hydrogen—air turbulent swirling premixed flames considering two swirl number and two equivalence ratio cases. Statistical characteristics of HRR are investigated by examining the mean HRR conditioned on a reaction progress variable and the total HRR in the computational domain. Conditional means of the HRR show that the magnitude of the HRR in reaction zones is smaller for higher swirl number cases than that for lower swirl number cases. A direct comparison between strained laminar and swirling flames shows the influence of the strain rate on the flame structure and the progress of elementary reactions. As strain rate increases in a laminar flame, the peak of the HRR by an exothermic reaction H2 + OH → H2O + H shifts toward the burnt side, implying active production of H in the burnt side. The HRR of the above reaction also shows an increasing tendency in a laminar flame under the strain rates greater than 106 s− 1. The strain–flame interaction with this tendency affects the HRR on highly strained flame surfaces of the swirling flames. It is also clarified that the local HRR intensity is dominated not only by strain rate but also by diffusion of H from the burnt to unburnt side.
机构:
Science and Technology on Scramjet Laboratory, College of Aerospace Science and Engineering, National University of Defense Technology, ChangshaScience and Technology on Scramjet Laboratory, College of Aerospace Science and Engineering, National University of Defense Technology, Changsha
Hu Y.
Tan J.-G.
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Science and Technology on Scramjet Laboratory, College of Aerospace Science and Engineering, National University of Defense Technology, ChangshaScience and Technology on Scramjet Laboratory, College of Aerospace Science and Engineering, National University of Defense Technology, Changsha
Tan J.-G.
Lv L.
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Science and Technology on Scramjet Laboratory, College of Aerospace Science and Engineering, National University of Defense Technology, ChangshaScience and Technology on Scramjet Laboratory, College of Aerospace Science and Engineering, National University of Defense Technology, Changsha
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UCL, Dept Mech Engn, London WC1E 7JE, EnglandUCL, Dept Mech Engn, London WC1E 7JE, England
Wang, Xujiang
Jin, Tai
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UCL, Dept Mech Engn, London WC1E 7JE, England
Zhejiang Univ, State Key Lab Clean Energy Utilizat, Hangzhou 310027, Zhejiang, Peoples R ChinaUCL, Dept Mech Engn, London WC1E 7JE, England
Jin, Tai
Luo, Kai H.
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UCL, Dept Mech Engn, London WC1E 7JE, EnglandUCL, Dept Mech Engn, London WC1E 7JE, England
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Xi An Jiao Tong Univ, State Key Lab Multiphase Flow Power Engn, Xian 710049, Peoples R China
Lund Univ, Div Fluid Mech, S-22100 Lund, SwedenXi An Jiao Tong Univ, State Key Lab Multiphase Flow Power Engn, Xian 710049, Peoples R China
Ji, Longjuan
Wang, Jinhua
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Xi An Jiao Tong Univ, State Key Lab Multiphase Flow Power Engn, Xian 710049, Peoples R ChinaXi An Jiao Tong Univ, State Key Lab Multiphase Flow Power Engn, Xian 710049, Peoples R China
Wang, Jinhua
Zhang, Weijie
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Xi An Jiao Tong Univ, State Key Lab Multiphase Flow Power Engn, Xian 710049, Peoples R ChinaXi An Jiao Tong Univ, State Key Lab Multiphase Flow Power Engn, Xian 710049, Peoples R China
Zhang, Weijie
Wang, Yuncheng
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Xi An Jiao Tong Univ, State Key Lab Multiphase Flow Power Engn, Xian 710049, Peoples R ChinaXi An Jiao Tong Univ, State Key Lab Multiphase Flow Power Engn, Xian 710049, Peoples R China
Wang, Yuncheng
Huang, Zuohua
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Xi An Jiao Tong Univ, State Key Lab Multiphase Flow Power Engn, Xian 710049, Peoples R ChinaXi An Jiao Tong Univ, State Key Lab Multiphase Flow Power Engn, Xian 710049, Peoples R China
Huang, Zuohua
Bai, Xue-Song
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Lund Univ, Div Fluid Mech, S-22100 Lund, SwedenXi An Jiao Tong Univ, State Key Lab Multiphase Flow Power Engn, Xian 710049, Peoples R China