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Experiment of Cooling-film Flows in a Hot-fire Environment

Experiment of Cooling-film Flows in a Hot-fire Environment

作     者:M.Q.Zhang 1 G.H.Yang 2 L.X.Zhou 2 L.Hong 2 Z.L.Zhang 2 1 Northwestern Polytechnical University Xi’an 710072 China 2 Xi’an Aerospace Propulsion Institute Xi’an 710100 China 

会议名称:《第六届国际流体力学会议》

会议日期:2011年

学科分类:080703[工学-动力机械及工程] 082502[工学-航空宇航推进理论与工程] 08[工学] 0807[工学-动力工程及工程热物理] 0825[工学-航空宇航科学与技术] 

关 键 词:film-cooling liquid rocket engine numerical simulation optical diagnostics gas-liquid interface 

摘      要:Experimental and numerical investigations on a cooling liquid-film flow in a hot-fire environment within a model combustion chamber were carried out to characterize the flow and heat transfer phenomena and to provide insight into flowfield and guide the evolution of the cooling design.A model combustion chamber with optical windows was set up for shadowgraph imaging of the liquid *** simulations using a separate-phase VOF method of the liquid-film flow and the combustion of the gaseous oxygen and methane were conducted to characterize the cooling-film flow and heat transfer between the hot combustion products and the liquid film.

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