期刊文献+

基于改进PMV指标的飞机驾驶舱热舒适性分析 被引量:9

Analysis of thermal comfort in aircraft cockpit based on the modified PMV index
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摘要 由于飞机驾驶舱处于高空太阳辐射的狭小热环境中,现有的人体热舒适性评价指标无法准确评价其热舒适性。本文从人体热平衡方程出发,对人体热舒适性预测平均评价(PMV)指标中的辐射换热项进行了修正,提出了一种适用于飞机驾驶舱内部热舒适性评价的指标PMV_F(PMV for Fighter)。同时,采用雷诺平均Navier-Stokes(RANS)方法对驾驶舱内部气流组织进行了数值计算,并对其热舒适性进行了分析。计算结果与实验数据吻合较好,基于PMV_F指标的计算结果能够反映驾驶舱内飞行员的热舒适状况,表明该方法可以用于飞机驾驶舱的热舒适性设计与评价。 To measure the thermal comfort of an aircraft cockpit with narrow space and high solar radiation for the pilot in the sky,the predicted mean vote(PMV)index has been studied in this paper.By increasing the effect of solar radiation in the human heat balance equation,an improved evaluation index PMV_F(PMV for Fighter)has been suggested in this paper.Meanwhile,numerical simulations as to an aircraft cockpit's flow field and temperature field have been taken by Reynolds average Navier-Stokes(RANS)method.The numerical simulation results are in a good agreement with the experimental data.The results of the PMV_F fit well with the status of pilot's thermal comfort.It shows that the method of numerical simulation based on the new evaluation index PMV_F can be used to analyze the thermal comfort in aircraft cockpit.
出处 《航空学报》 EI CAS CSCD 北大核心 2015年第3期819-826,共8页 Acta Aeronautica et Astronautica Sinica
基金 江苏高校优势学科建设工程资助项目~~
关键词 热舒适性 PMV 评价指标 飞机驾驶舱 数值计算 thermal comfort PMV evaluation index aircraft cockpit numerical simulation
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参考文献17

  • 1Fanger P O. Calculation of thermal comfort [ J ]. ASHRAETransactions 1966, 73(3) : 1-20.
  • 2Fanger P O. Thermal comfort[M]. New York: McGrawHill,1972.
  • 3Mezrhab A,Bouzidi M. Computation of thermal comfortinside a passenger car compartment [J]. Applied ThermalEngineering, 2006, 26(14-15): 1697-1704.
  • 4杨培志,陈焕新.热舒适评价指标PMV-PPD在空调列车上的应用[J].制冷空调与电力机械,2002,23(2):22-24. 被引量:15
  • 5Gunther G,Bosbach J, Julien P. Experimental and nu-merical simulation of idealized aircraft cabin flows [ J].Aerospace Science and Technology , 2006, 10(7) : 563-573.
  • 6Lin C H, Dunn K H,Horstman R H. Numerical simula-tion of airflow and airborne pathogen transport in aircraftcabins-part(I) : numerical simulation of the flow field[J].ASHRAE Transactions, 2005 . 111(1) ; 755-763.
  • 7Zhang T F, Chen Q Y. Novel air distribution systems forcommercial airecraft cabins [J]. Building and Environ-ment, 2007, 42(4) : 1675-1684.
  • 8袁修干.飞机座舱热力学特性的数学模型及其应用[J]北京航空学院学报,1982,4:47-59.
  • 9吴玉庭,林国华,袁修干.空调座舱热舒适性计算[J].北京航空航天大学学报,2000,26(1):56-59. 被引量:11
  • 10吴丹,许常悦,孙建红.来流马赫数对座舱气动加热影响的数值模拟[J].南京航空航天大学学报,2011,43(4):464-469. 被引量:4

二级参考文献40

  • 1徐远清,陈祥光,王丽,朱铁丹.一种基于模糊因果聚类的室内热舒适预测方法[J].仪器仪表学报,2006,27(z1):850-852. 被引量:3
  • 2艾永冠,朱卫东,闫冬.基于PSO-BP神经网络的股市预测模型[J].计算机应用,2008,28(S2):105-108. 被引量:11
  • 3李仁欣,唐世君.穿着服装热舒适性的预测模型和应用[J].航天医学与医学工程,1994,7(4):258-265. 被引量:6
  • 4赵荣义,许为全.改善室内空气环境的调节策略[J].暖通空调,1997,27(1):1-4. 被引量:16
  • 5黎作武,张涵信.高超声速航天飞行器气动热特性的数值模拟[C]//第十届全国计算流体力学会议论文集.2000:103-108.
  • 6[1]Letlow J T,Jewkins L C .Development of an integrated environmental control system.SAE981544,1998.
  • 7[3]Lui C W,Lee C K,Schwan E.Integrated environmental control system and liquid cooling system for F/A-18E/F.SAE951400,1995.
  • 8Holden M S, Wadhams T P. A database of aerother- mal measurements in hypersonic flow in " Building Block" experiments for CFD validation[R]. AIAA paper 2003-1137, 2003.
  • 9Nichols R H, Nelson C C. Wall function boundary conditions including heat transfer and compressibility for transport"turbulence models [R]. AIAA paper 2004-582, 2004.
  • 10Scherrer R. Comparison of theoretical and experi- mental heat-transfer characteristics of bodies of revo- lution at supersonic speeds[R]. NACA-RM-ASL28, 1950.

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