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实验动物房压差数值模拟与分析 被引量:1

Simulation and Analysis for Air Differential Control of Laboratory Animal Room
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摘要 为了保证实验动物饲养环境达到相应的标准,需要实验动物房相对外界保持一定的正压。本文模拟分析了实验动物房的内外环境空气压差,首先对迎风面上的压强进行了模拟,总结了迎风面压强变化函数;同时对室内房间之间的压差梯度进行了详细分析;最后总结了为保障其室内外的气流环境安全所必须采取的措施。 In order to guarantee the laboratory animal room air environment security, positive pressure need to keep the indoor between the outdoor. In this paper, pressure differential of laboratory animal room was simulated and analyzed. At first, the pressure differential on the windward side was simulated; the function of the pressure differential on the windward side was draw; at the same time, the pressure differential among the indoor rooms was analyzed detailed; at last, the way to protect the laboratory animal room air environment security was draw.
出处 《建筑热能通风空调》 2012年第3期63-66,43,共5页 Building Energy & Environment
基金 湖南省教育厅项目(11C1100)
关键词 实验动物房 空气环境 数值模拟 laboratory animal room, air environment, numerical simulation
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参考文献10

  • 1国家质量技术监督局.实验动物环境与设施(GB14925-2001)[S].2002.
  • 2张相庭.结构风压和风振计算[M].上海:同济大学出版社,1984.
  • 3武文斐,李义科,符永正.建筑物表面风压分布随迎风面宽度变化的数值模拟[J].工业建筑,1997,27(1):54-57. 被引量:3
  • 4Jiang Xinbo, Liu Zehua, Liu Yuanquan. Air environment in a laboratory animal room under different pressure differentials [A]. In: The Fifth International Workshop on Energy and Environment of Residential Buildings [C]. Guilin, 2009.931-936.
  • 5Jiang Xinbo, Liu Zehua, Hartmori Yoshida, et al. Pressure differe- ntial analysis of a laboratory animal room [A]. In: Maximizing Building Energy Efficiency and Comfort (Part 2) [C]. Shenzhen, 2006.820-826.
  • 6K Yamagutsi. Basic Research of Indoor Air Distribution [D]. Osaka: Osaka University, 1979.
  • 7包涵龄,陈鹏,武玉英.用不同湍流模型预测机翼边界层分离区[J].北京工业大学学报,2003,29(2):159-163. 被引量:5
  • 8包涵龄.边界层分离流边值问题的算法研究[J].空气动力学学报,1998,16(4):468-472. 被引量:4
  • 9V I Voronin, G S Ulyanov, A I Shvetz. Experimental study of supersonic flow past wedges with longitudinal grooves on the windward side [J]. Fluid Dynamics, 1993, 28( 2): 296-298.
  • 10Concentration, Heat and Momentum Limited [Z]. PHOENICS Week Training Materials, 2003.

二级参考文献16

  • 1袁礼,忻鼎定.湍流应力模式对计算有分离三维边界层的效果研究[J].空气动力学学报,1994,12(2):130-138. 被引量:2
  • 2包涵龄.计算实际机翼湍流边界层流动的积分法[J].空气动力学学报,1988,6(4):491-496.
  • 3CEBECI T, KHALIC E E, WH1TELAW J H. Calculation of separated boundary layer flows[J]. 1979,AIAA-79-0284.
  • 4ROTrA R C. A family of turbulence models for three dimensional boundary layers[A]. Turbulent Shear Flows vol Ⅱ[M]. New York: Springer-Verlag, 1979.
  • 5van den BERG B, ELSENNAR A. Measurements in a 3-D incompressible turbulent boundary layer in an adverse pressure gradient under infinite swept wing conditions[J]. 1972, NLR TR 72092U.
  • 6SMITH P D. A calculation method for the turbulent boundary layer on an infinite yawed wing in compressible adiabatic flow[J]. 1972, ARC R&M 3739.
  • 7RODI W. Experience with two-layer models combining the κ-ε model with a one-equation model near the wall[J].1991, AIAA-91-0216.
  • 8CHEN H C, PATEL V C. Near-wall turbulence models for complex flows including separation[J]. AIAA Journal,1988, 26: 641-648.
  • 9包涵龄.机翼边界层计算及其在飞机设计中的应用[J].航空学报,1987,8(11):553-560.
  • 10包涵龄,空气动力学学报,1998年,16卷,2期

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