Xiaowei Luo, Ph.D. - Publications

Affiliations: 
2000 Stanford University, Palo Alto, CA 
Area:
Comparative and Historical Sociology, Organizations and Work, Political Sociology, Sociology of Education

71 high-probability publications. We are testing a new system for linking publications to authors. You can help! If you notice any inaccuracies, please sign in and mark papers as correct or incorrect matches. If you identify any major omissions or other inaccuracies in the publication list, please let us know.

Year Citation  Score
2016 Ma J, Luo X, Li H, Liu Y. An experimental investigation on transpiration cooling based on the multilaminated sintered woven wire mesh structures Journal of Thermal Science and Engineering Applications. 8. DOI: 10.1115/1.4032921  0.36
2016 Liu D, Tao Z, Luo X, Wu H, Yu X. Development of a New Factor for Hot Gas Ingestion Through Rim Seal Journal of Engineering For Gas Turbines and Power. 138. DOI: 10.1115/1.4031758  0.36
2016 Xie B, Hu R, Yu X, Shang B, Ma Y, Luo X. Effect of Packaging Method on Performance of Light-Emitting Diodes with Quantum Dot Phosphor Ieee Photonics Technology Letters. 28: 1115-1118. DOI: 10.1109/LPT.2016.2531794  0.36
2016 Luo X, Feng A, Quan Y, Zhou Z, Liao N. Experimental analysis of varied vortex reducers in reducing the pressure drop in a rotating cavity with radial inflow Experimental Thermal and Fluid Science. 77: 159-166. DOI: 10.1016/j.expthermflusci.2016.04.011  0.36
2016 Liu D, Tao Z, Luo X, Kang W, Yu X. Application of heat and mass transfer analogy on hot gas ingestion through rim seal Applied Thermal Engineering. 102: 622-632. DOI: 10.1016/j.applthermaleng.2016.03.023  0.36
2016 Ma J, Lv P, Luo X, Liu Y, Li H, Wen J. Experimental investigation of flow and heat transfer characteristics in double-laminated sintered woven wire mesh Applied Thermal Engineering. 95: 1-9. DOI: 10.1016/j.applthermaleng.2015.11.015  0.36
2015 Luo X, Zhang D, Xu GQ. Experimental study on windage torque in unshrouded rotor-stator system with central inflow Tuijin Jishu/Journal of Propulsion Technology. 36: 1199-1205. DOI: 10.13675/j.cnki.tjjs.2015.08.012  0.36
2015 Zhang D, Luo X, Xu GQ, Han JQ. Windage heating experiment on rotating disc in cavity of rotor-stator system Hangkong Dongli Xuebao/Journal of Aerospace Power. 30: 1047-1056. DOI: 10.13224/j.cnki.jasp.2015.05.004  0.36
2015 Cai X, Luo X, Zhao X, Xu GQ, Cai J. Flow characteristics in a rotor-stator cavity with cooling air inlet at low radius Hangkong Dongli Xuebao/Journal of Aerospace Power. 30: 775-783. DOI: 10.13224/j.cnki.jasp 2015.04.002  0.36
2015 Liang Z, Luo X, Feng Y, Xu G. Experimental investigation of pressure losses in a co-rotating cavity with radial inflow employing tubed vortex reducers with varied nozzles Experimental Thermal and Fluid Science. 66: 304-315. DOI: 10.1016/j.expthermflusci.2015.03.008  0.36
2014 Tao Z, Zhang D, Luo X, Xu G, Han J. Windage Heating in a Shrouded Rotor-Stator System. Journal of Engineering For Gas Turbines and Power. 136: 0626021-6260210. PMID 25805919 DOI: 10.1115/1.4026429  0.36
2014 Zhan WB, Xu GQ, Quan YK, Luo X, Li TT. Design and analysis of a novel hybrid solar/gas dish stirling system (HS/GDSS) Applied Mechanics and Materials. 479: 575-579. DOI: 10.4028/www.scientific.net/AMM.479-480.575  0.36
2014 Zhang D, Luo X, Xu G, Tian S. Windage measurements for rotating disc with protrusions Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics. 40: 1055-1059. DOI: 10.13700/j.bh.1001-5965.2013.0536  0.36
2014 Zhang D, Han JQ, Luo X, Xu GQ. Numerical simulation of friction torque of rotating disc for rotor-stator system with central inflow Hangkong Dongli Xuebao/Journal of Aerospace Power. 29: 755-762. DOI: 10.13224/j.cnki.jasp.2014.04.003  0.36
2014 Luo X, Liu D, Wu H, Tao Z. Particle image velocimetry measurement and computational fluid dynamic simulations of the unsteady flow within a rotating disk cavity Journal of Engineering For Gas Turbines and Power. 136. DOI: 10.1115/1.4027568  0.36
2014 Luo X, Zhang D, Tao Z, Xu G, Wang Q. Windage measurements in a rotor-stator system with superimposed cooling and rotor-mounted protrusions Journal of Engineering For Gas Turbines and Power. 136. DOI: 10.1115/1.4026086  0.36
2014 Luo X, Han G, Wu H, Wang L, Xu G. Experimental investigation of pressure loss and heat transfer in a rotor-stator cavity with two outlets International Journal of Heat and Mass Transfer. 78: 311-320. DOI: 10.1016/j.ijheatmasstransfer.2014.06.057  0.36
2014 Luo X, Wang L, Zhao X, Xu G, Wu H. Experimental investigation of heat transfer in a rotor-stator cavity with cooling air inlet at low radius International Journal of Heat and Mass Transfer. 76: 65-80. DOI: 10.1016/j.ijheatmasstransfer.2014.04.013  0.36
2014 Luo X, Zhao X, Wang L, Wu H, Xu G. Flow structure and heat transfer characteristics in rotor-stator cavity with inlet at low radius Applied Thermal Engineering. 70: 291-306. DOI: 10.1016/j.applthermaleng.2014.05.006  0.36
2013 Li D, Luo X, Cai X. Method for measuring pressure under rotating conditions Advanced Materials Research. 663: 522-527. DOI: 10.4028/www.scientific.net/AMR.663.522  0.36
2013 Ning B, Luo X, Feng Y, Chen X, Wu LJ. Study on total pressure losses characteristics of rotating cavity with radial inflow of different Drum Hole Shape Advanced Materials Research. 663: 483-489. DOI: 10.4028/www.scientific.net/AMR.663.483  0.36
2013 Zhang LJ, Luo X, Yu HP, Guo J. Experiment on gas ingestion on forward disk cavity of 1.5 stage turbine rig Hangkong Dongli Xuebao/Journal of Aerospace Power. 28: 2746-2751.  0.36
2013 Cai X, Luo X, Xu GQ, Li DC, Huang YZ. Experiment on pressure characteristics of dual rotating cavities Hangkong Dongli Xuebao/Journal of Aerospace Power. 28: 2267-2275.  0.36
2013 Zhao X, Xu GQ, Luo X, Feng Y, Wang L. Effects on calibration and use of thermochromic liquid crystal Hangkong Dongli Xuebao/Journal of Aerospace Power. 28: 1409-1414.  0.36
2012 Dong B, Xu G, Luo X, Cai Y, Gao W. A bibliometric analysis of solar power research from 1991 to 2010 Scientometrics. 93: 1101-1117. DOI: 10.1007/s11192-012-0730-9  0.36
2012 Yu X, Lu HY, Sun JN, Luo X, Xu GQ. Study of the pressure drop for radial inflow between co-rotating discs 28th Congress of the International Council of the Aeronautical Sciences 2012, Icas 2012. 4: 2828-2832.  0.36
2012 Luo X, Feng Y, Xu GQ, Zhao X, Zhao N. Numerical simulation of flow and heat transfer performances in a direct transfer pre-swirl system Hangkong Dongli Xuebao/Journal of Aerospace Power. 27: 2188-2193.  0.36
2012 Xu GQ, Zhao X, Luo X, Cai X, Yu HP. Heat transfer in direct transfer pre-swirl rotor-stator system Hangkong Dongli Xuebao/Journal of Aerospace Power. 27: 2161-2168.  0.36
2012 Cai X, Xu GQ, Luo X, Zhao X, Li Y. Experiment of flow characteristics of direct transfer pre-swirl system Hangkong Dongli Xuebao/Journal of Aerospace Power. 27: 2222-2228.  0.36
2012 Sun JN, Luo X, Liu JN, Xu GQ, Zhou ZX, Qiu CB. Volume fraction technique for measuring the minimum value of mass flow in turbine rotor-stator disk cavities Hangkong Dongli Xuebao/Journal of Aerospace Power. 27: 981-985.  0.36
2012 Sun JN, Luo X, Liu JN, Xu GQ, Zhou ZX, Qiu CB. Transient measurement for measuring the heat transfer in a rotating cavity with a high rotational speed Hangkong Dongli Xuebao/Journal of Aerospace Power. 27: 969-974.  0.36
2011 Zhou KY, Luo X, Xu GQ. Numerical simulation of rotationally-induced ingress through turbine rim seals Hangkong Dongli Xuebao/Journal of Aerospace Power. 26: 2704-2709.  0.36
2011 Quan YK, Xu GQ, Luo X, Zhang D. Development and calibration of heat transfer coefficient sensor for rotational state Hangkong Dongli Xuebao/Journal of Aerospace Power. 26: 2684-2690.  0.36
2011 Liu XH, Tao Z, Luo X. Experimental investigation on effect of small auxiliary holes on film cooling effectiveness Hangkong Dongli Xuebao/Journal of Aerospace Power. 26: 2710-2715.  0.36
2011 Yu K, Luo X, Wen J. Heat transfer study on a turbine rotor endwall by an improved transient experiment method Hangkong Dongli Xuebao/Journal of Aerospace Power. 26: 1975-1980.  0.36
2011 Zhao X, Xu GQ, Luo X. Effects of temperature distribution and level on heat transfer on a rotating free disk Hangkong Dongli Xuebao/Journal of Aerospace Power. 26: 1310-1320.  0.36
2011 Li FQ, Luo X, Xu GQ. Experimental study of flow friction characteristics for a rotor-stator system with centre inflow of cooling air Hangkong Dongli Xuebao/Journal of Aerospace Power. 26: 1334-1340.  0.36
2010 Yu X, Luo X, Sun JN, Xu GQ, Deng HW, Shen EN. PIV measurements of the flow in a rotating cavity with a radial inflow Heat Transfer Research. 41: 787-799. DOI: 10.1615/HeatTransRes.v41.i7.70  0.36
2010 Liu X, Luo X, Tao Z. Effects of cylindrical hole accompanied with anti-vortex holes on film cooling effectiveness Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics. 36: 1271-1274+1280.  0.36
2010 Liu XH, Luo X, Tao Z. Analysis on improvement of film cooling effectiveness with small coolant jets Hangkong Dongli Xuebao/Journal of Aerospace Power. 25: 2267-2272.  0.36
2010 Deng H, Tan Y, Wang J, Luo X. Flow and heat transfer in the complex passages of turbine blade trailing edge Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics. 36: 1013-1016.  0.36
2010 Ding S, Jiang Z, Xu G, Luo X. Transient measurement of heat transfer coefficient Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics. 36: 883-886.  0.36
2010 Deng HW, Ma M, Luo X. Film deflection measurements of a rotating film cooling model Hangkong Dongli Xuebao/Journal of Aerospace Power. 25: 724-728.  0.36
2010 Zhao X, Xu GQ, Tao Z, Luo X. Effect of temperature level on heat transfer on a free disk with laminar flow Hangkong Dongli Xuebao/Journal of Aerospace Power. 25: 503-508.  0.36
2010 Quan YK, Sun JN, Luo X. Pressure measurements on a static disk with high positioned inflow and radial outflow under rotor-stator system Hangkong Dongli Xuebao/Journal of Aerospace Power. 25: 53-57.  0.36
2009 Wang YJ, Xu GQ, Deng HW, Luo X. Experimental investigation on heat transfer of supercritical RP-3 Tuijin Jishu/Journal of Propulsion Technology. 30: 656-660.  0.36
2009 Quan Y, Xu G, Luo X, Ding S. Development of kind of heat transfer coefficient sensor based on steady method Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics. 35: 1413-1416.  0.36
2009 Yu X, Luo X, Xu GQ, Sun JN. Particle image velocimetry (PIV) measurements of the flow in a rotating cavity with a radial inflow Hangkong Dongli Xuebao/Journal of Aerospace Power. 24: 2483-2488.  0.36
2009 Wang YJ, Xu GQ, Wu HW, Deng HW, Luo X. Experimental investigation of RP-3 thermal oxidation stability Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics. 30: 1710-1712.  0.36
2009 Wang YJ, Xu GQ, Deng HW, Luo X, Wang Q. Experimental study of influence of inlet temperature on aviation kerosene coking characteristics Hangkong Dongli Xuebao/Journal of Aerospace Power. 24: 1972-1976.  0.36
2009 Zhao X, Xu G, Luo X, Deng H. Cooling structure on double-web turbine disk with equal mass scheme Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics. 35: 527-531.  0.36
2008 Tao Z, Yang X, Ding S, Xu G, Wu H, Deng H, Luo X. Experimental study of rotation effect on film cooling over the flat wall with a single hole Experimental Thermal and Fluid Science. 32: 1081-1089. DOI: 10.1016/j.expthermflusci.2007.12.003  0.36
2008 Yang B, Xu G, Ding S, Luo X. Numerical study of film cooling characteristics on a rotating turbine blade model Hangkong Xuebao/Acta Aeronautica Et Astronautica Sinica. 29: 274-279.  0.36
2008 Wu H, Meng H, Luo X, Xu G. Heat transfer enhancement characteristics in nature convection along vibrant surface Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics. 34: 307-310.  0.36
2007 Luo X, Xu GQ, Tao Z, Ding ST. Cooling effectiveness in a rotor-stator system with different pre-swirl angles Tuijin Jishu/Journal of Propulsion Technology. 28: 240-243.  0.36
2007 Luo X, Xu GQ, Cai Y, Tao Z, Ding ST. Experimental study of flow distribution characteristics for a rotor-stator system Hangkong Dongli Xuebao/Journal of Aerospace Power. 22: 873-876.  0.36
2007 Luo X, Xu GQ, Cai Y, Tao Z, Ding ST. Influence of central outflow on flow and heat transfer in a pre-swirl rotor-stator system Hangkong Dongli Xuebao/Journal of Aerospace Power. 22: 709-713.  0.36
2007 Yang XJ, Tao Z, Ding ST, Xu GQ, Luo X. Analysis of curvature effects on the film cooling under the rotation frame Hangkong Xuebao/Acta Aeronautica Et Astronautica Sinica. 28: 540-544.  0.36
2007 Xu GQ, Tian N, Tao Z, Ding ST, Luo X, Deng HW. Experimental research on flat surface film cooling by TLC Hangkong Dongli Xuebao/Journal of Aerospace Power. 22: 704-708.  0.36
2007 Luo X, Xu G, Tao Z, Ding S. Flow and heat transfer in rotor-stator system with pre-swirl angle of 30° Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics. 33: 290-293.  0.36
2007 Tao Z, Gao J, Cai Y, Ding ST, Luo X, Zou ZP. Experimental investigation of the flow field between a rotating and a stationary disk at high-positioned air inflow Hangkong Dongli Xuebao/Journal of Aerospace Power. 22: 347-351.  0.36
2006 Wu H, Lei B, Cai Y, Luo X, Zhang S. Experimental investigation on frictional loss in shrouded rotating disk with high-positioned air inflow Hangkong Dongli Xuebao/Journal of Aerospace Power. 21: 1008-1011.  0.36
2006 Xu GQ, Zhang S, Luo X, Ding ST, Tao Z, Lei B. Experimental investigation on heat transfer in shrouded rotating disk with high-positioned air inflow Hangkong Dongli Xuebao/Journal of Aerospace Power. 21: 820-823.  0.36
2006 Luo X, Xu GQ, Tao Z, Ding ST. Cooling effectiveness of a rotating disk with discrete receiver holes Hangkong Dongli Xuebao/Journal of Aerospace Power. 21: 621-625.  0.36
2006 Luo X, Xu G, Tao Z, Ding S. Heat transfer measurements on a rotating disk with discrete receiver holes Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics. 32: 922-925.  0.36
2005 Zhang C, Luo X, Xu G, Tao Z. Experimental study of static pressure characteristics at stator surface in a rotor-stator disk cavity Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics. 31: 385-388.  0.36
2004 Luo X, Zhang C, Xu G, Tao Z, Ding S. Measurements of surface temperature distribution on a rotating disk with blade cooling holes using thermochromic liquid crystal Proceedings of the Asme Turbo Expo 2004. 4: 365-371.  0.36
2004 Luo X, Xu G, Ding S, Tao Z. Experimental investigation on transient heat transfer in rotor-stator system with high-positioned air inflow Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics. 30: 512-515.  0.36
2000 Xu GQ, Zhan ZG, Ding ST, Tao Z, Luo X. Comparision of cooling effectiveness between central and high-positioned air inlet rotor-stator disk systems Tuijin Jishu/Journal of Propulsion Technology. 21: 43-44.  0.36
2000 Xu Gq, Zhan Zg, Ding St, Tao Z, Luo X. Comparison of cooling effectiveness between central and high-positioned air inlet rotor-stator disk systems Tuijin Jishu/Journal of Propulsion Technology. 21: 42-44.  0.36
2000 Xu GQ, Zhan GZ, Ding ST, Tao Z, Luo X. Numerical calculation for flow and heat transfer of a shrouded rotating disk with high-positioned air-inlet Tuijin Jishu/Journal of Propulsion Technology. 21: 42-43.  0.36
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