期刊文献+

高温气固两相流风洞的设计 被引量:3

Wind Tunnel Design of High-temperature Gas-solid Two-phase Flow
下载PDF
导出
摘要 为了模拟锅炉燃烧过程中的气固两相流流动工况,更好地研究其流动特性及测试方法,设计了高温气固两相流风洞。确定了风洞的主要技术参数及其控制回路。重点介绍了风洞的结构设计,其中以收缩段和进料装置的设计最为关键,借助Fluent软件对颗粒运动轨迹进行了数值模拟。计算结果表明:该设计方案能够保证试验段气固两相流的均匀性和稳定性。 A wind tunnel has been designed for simulating the working condition of gas-solid two-phase boiler combustion processes so as to study the flow characteristics and work out reasonable test methods. parameters of the tunnel and its control loop components such as the contraction section and flows formed in Main technical are determined, with focus on the structural design, including key feeding on moving tracks of particles is carried out. Calculation device. By making use of Fluent software, numerical simulation results show that the design can guarantee evenness and stability of the two-phase flow section tested. Figs 3 and refs 9.
出处 《动力工程》 EI CSCD 北大核心 2007年第1期95-98,共4页 Power Engineering
基金 浙江大学宁波理工学院科研启动基金资助项目
关键词 工程热物理 风洞 高温气固两相流 试验段 收缩段 数值模拟 engineering thermophysics wind tunnel high-temperature gas-solid two-phase flow test section contraction section numerical simulation
  • 相关文献

参考文献9

二级参考文献14

  • 1颜大椿.大型冷却塔群风载问题的风洞模拟.中国力学学会第三届全国流体力学学术会议论文集[M].科学出版社,1988.. 被引量:1
  • 2解亚军.FL-9风洞收缩段初步气动设计说明[R].西北工业大学翼型研究中心科技报告,.. 被引量:1
  • 3焦予秦.[D].西北工业大学,2001. 被引量:1
  • 4VATSA V N, WEDAN B W. Navier-Stokes solutions for transonic flow over a wing mounted in a tunnel [ R ]. MAA 88-0102,1988. 被引量:1
  • 5JAMSON A, SCHMIDT W, TURKEL E. Numerical solution of Euler equations by finite volume methods with Runge-Kutta time stepping schemes[R] .AIAA 81-12.59, 1981. 被引量:1
  • 6JAMSON A, BAKER T J. Solution of the Elder equations for complex configurations[R]. AIAA 83-1929,1983. 被引量:1
  • 7VATSA V N. Accurate numerical simulations for transonic viscons flow over finite wing [J]. J. Aircraft, 1987,24 ( 6 ). 被引量:1
  • 8VATSA V N, et al.. Navier-Stokes computations of prolate spheroids at angle of attack [R]. AIA.A 87-2627-CP, 1987. 被引量:1
  • 9LINDEBERG T. The construction of a three-dimensional finite volume grid generator for a wing in a wind tunnel with application to Navier-Stokes flow solvers[R]. FFA TN 1987-58,1987. 被引量:1
  • 10WII,I,IAM C ROSE. Numerical investigation in three-dimensional internal flows [R]. Semi-Annul Status Report, University of Nevada, Dec. 1990. 被引量:1

共引文献65

同被引文献16

  • 1李华星,贺家驹,左培初,徐敏.柔壁自适应风洞低超音速实验技术研究[J].航空学报,1993,14(7). 被引量:1
  • 2赵鸣志,浦兴国,周洁,袁镇福.高温两相流风洞收缩段和试验段的数值模拟研究[J].中国电机工程学报,2006,26(9):50-53. 被引量:7
  • 3冯冬青,谢宋和,等.模糊智能控制[M].北京:化学工业出版社,2002. 被引量:2
  • 4中国人民解放军总装备部军事训练教材编辑委员会编.高低速风洞气动与结构设计[M].北京:国防工业出版社,2003:186-187. 被引量:2
  • 5曾丹苓,敖越,朱克雄.工程热力学(第二版)[M].北京:高等教育出版社,1985:334-337. 被引量:2
  • 6Inoue K, Aso S. A study on new ramp injectors with slotted nozzle for improvement of supersonic mixing[C]. 40th AIAA/ASME/ SAE/ASEE Joint Propulsion Conference and Exhihit, Fort Lauder- dale, Florida , 2004, July 11-14. 被引量:1
  • 7William J Nelson, James M Cubbage. Effects of slot size and geome- try on the flow in rectangular tunnels at Mach number up to 1. 4 [R]. NACA RM, 1957. 被引量:1
  • 8Kei Inoue, Shigeru kso, Shingo Kawano. Effects of injection angle of slotted nozzle on supersmlic mixing[J]. Computational Fluid Dy- namics Journal, 2004, 13(2) : 266-272. 被引量:1
  • 9何乃波.跨声速变质量槽式喷管的设计及数值模拟[D].上海:上海理工大学,2010. 被引量:1
  • 10Moin P. Progress in large eddy simulation of turbulence flows[J]. AIAA Journal, 1997, 38(2): 750-761. 被引量:1

引证文献3

二级引证文献5

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部