Experimental and numerical studies have been conducted to investigate the flow field and heat transfer characteristics of a pair of counter rotating dual-swirling flames impinging on a flat surface. Effect of separation distance (H/D-h 3, 4, 6 and 8), inter-jet spacings (S/D-h - 4, 7 and 10) and Reynolds number on flow interactions and impingement heat transfer have been studied under stoichiometric conditions. The inner non-swirling flames are seen to bend towards interacting side due to asymmetric interactions developed in a pair of dual-swirling flames. Commercial computational fluid dynamics (CFD) code (FLUENT (R)) has been used to simulate the interacting dual-swirling impinging flames. Numerical simulation predicted the deflection of inner flames to be primarily due to large distorted RCZ developed from asymmetric interactions. Comparisons of co-and-counter swirling configurations suggest that the presence of plate has a stronger influence on flow structure of impinging flames than sign of rotation. High resolution heat fluxes have been obtained using steady state 1-D heat balance from temperature readings obtained on rear side of quartz impingement plate through IR thermal camera. 1-D heat balance has been corrected for lateral conduction taking place inside the impingement plate using an iterative procedure. For counter swirl case, cross-flow leaves as a straight flow along the transverse direction due to the nature of interactions. Cross-flow causes heat flux contours in the interaction region to be asymmetric and preferential heating is observed along the transverse direction. The increase in Re(o) causes wider flame spread and severe interactions result in increased tendency for preferential heating of the impingement plate. High average heat fluxes are obtained at smallest H/Dh and S/Dh whereas minimum relative deviation is observed at S/D-h - 10 for H/D-h - 4.
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Xi An Jiao Tong Univ, State Key Lab Mfg Syst Engn, Xian 710049, Peoples R ChinaXi An Jiao Tong Univ, State Key Lab Mfg Syst Engn, Xian 710049, Peoples R China
Xu, Liang
Yang, Tao
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Xi An Jiao Tong Univ, State Key Lab Mfg Syst Engn, Xian 710049, Peoples R ChinaXi An Jiao Tong Univ, State Key Lab Mfg Syst Engn, Xian 710049, Peoples R China
Yang, Tao
Sun, Yanhua
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Xi An Jiao Tong Univ, State Key Lab Mfg Syst Engn, Xian 710049, Peoples R ChinaXi An Jiao Tong Univ, State Key Lab Mfg Syst Engn, Xian 710049, Peoples R China
Sun, Yanhua
Xi, Lei
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Xi An Jiao Tong Univ, State Key Lab Mfg Syst Engn, Xian 710049, Peoples R ChinaXi An Jiao Tong Univ, State Key Lab Mfg Syst Engn, Xian 710049, Peoples R China
Xi, Lei
Gao, Jianmin
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Xi An Jiao Tong Univ, State Key Lab Mfg Syst Engn, Xian 710049, Peoples R ChinaXi An Jiao Tong Univ, State Key Lab Mfg Syst Engn, Xian 710049, Peoples R China
Gao, Jianmin
Li, Yunlong
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Xi An Jiao Tong Univ, State Key Lab Mfg Syst Engn, Xian 710049, Peoples R ChinaXi An Jiao Tong Univ, State Key Lab Mfg Syst Engn, Xian 710049, Peoples R China
Li, Yunlong
Li, Jibao
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AECC Commercial Aircraft Engine Co LTD, Shanghai, Peoples R ChinaXi An Jiao Tong Univ, State Key Lab Mfg Syst Engn, Xian 710049, Peoples R China