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Investigation on the transpiration cooling of a liquid rocket nozzle
Jin Shao-shan ; Jiang Pei-xue ; Sun Ji-guo
2010-10-12 ; 2010-10-12
关键词Experimental/ aerodynamics cooling mass transfer nozzles propellants rocket engines transpiration turbulence/ liquid rocket Laval nozzle transpiration cooling SST k- omega turbulence model propellant rocket engine thermal disperse effect microscale flow mass transfer boundary layer thickness dimension aerodynamics formula/ A4785 Applied fluid mechanics A4725 Turbulent flows, convection, and heat transfer A4755E Nozzles A4740 Compressible flows shock and detonation phenomena A4755M Flow through porous media E2320 Engines E2200 Mechanical components, systems and devices E2130 Fluid mechanics and aerodynamics (mechanical engineering) E2120 Heat and thermodynamic processes (mechanical engineering)
中文摘要The SST k - omega turbulence model was used to simulate the coupled whole field of the transpiration cooling of a Laval-nozzle of a liquid O/sub 2//H/sub 2/ propellant rocket engine. The influences of porosity, variation property, compressibility, the thermal disperse effect of porous media, micro-scale flow and mass transfer were considered in the model. The influences of porosity on local blowing ratio, the wall temperature and the boundary layer thickness were analyzed and compared with the regenerative cooling. The results showed that the increase of average blowing ratio can decrease the average wall temperature with a larger proportion and for the transpiration cooling nozzle the throat is no longer the highest temperature point. The simulation results were compared with both the experimental results and the one dimension aerodynamics formula and approved to be accurate.
语种中文
出版者Editorial Department of the Journal of Aerospace Power ; China
内容类型期刊论文
源URL[http://hdl.handle.net/123456789/79981]  
专题清华大学
推荐引用方式
GB/T 7714
Jin Shao-shan,Jiang Pei-xue,Sun Ji-guo. Investigation on the transpiration cooling of a liquid rocket nozzle[J],2010, 2010.
APA Jin Shao-shan,Jiang Pei-xue,&Sun Ji-guo.(2010).Investigation on the transpiration cooling of a liquid rocket nozzle..
MLA Jin Shao-shan,et al."Investigation on the transpiration cooling of a liquid rocket nozzle".(2010).
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