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航空动力学报2016年8期

2023-02-20 06:44 来源:学术参考网 作者:未知

航空动力学报2016年8期

《航空动力学报》是由中国航空学会主办,中国航空一集团主管,北京航空航天大学承办的中文科技核心学术刊物。1986年7月创刊,创刊时为季刊,现为半月刊。向国内外公开发行。

航空动力学报的主要栏目

本刊设有航空航天发动机原理与设计、叶轮机械、燃烧、传热、传质、自动控制、结构、强度、振动、气动热力学、机械传动、实验技术等栏目。

航空动力学报的收录情况

国外:美国工程信息公司EI《Engineering Index》美国《国际航空宇航文摘》(International Aerospace Abstracts)美国《航空航天数据库(Aerospace Database)》美国剑桥科学文摘CSA (Cambridge Scientific Abstracts)英国《科学文摘》(SA,INSPEC)俄罗斯文摘杂志(AJ of VINITI)日本《科学技术文献速报》(CBST)(即JST,日本科学激素信息社数据库)波兰《哥白尼索引》(IC)国内:《中国科学院文献情报中心数据库》《中国学术期刊数据库(CNKI)》《中国学术期刊文摘》《航空航天数据库》《中国科技论文引文数据库(CSTP、CSTY)》《中国科学引文数据库(CSCD)》《中文科技期刊数据库(VIP)》《中国力学文摘数据库》《中国物理文摘数据库》《中国学术期刊(光盘版)》《中国期刊网》等并同英国皇家航空协会,美国AEROSPACE、AIAA等国外期刊进行交换。学报自创刊至今,共发表2500多篇文章,其中各种基金项目的文章占30%。

王建华的论文发表

[1] Wang J. H., Shi J. X., Discussion of Boundary Conditions of Transpiration Problems   Using LTNE Model, ASME J. of Heat Transfer, Jan. 2008,Vol.130, No.1. [2] Wang J. H., Wang H. N., A Discussion of Transpiration Cooling Problems Through an Analytical Solution of Local Thermal Non-Equilibrium Model, ASME J. of Heat Transfer, Oct. 2006, Vol. 128, 1093-1098.[3] Shi J. X., Wang J. H., Inverse problem of transpiration cooling for estimating wall heat flux by LTNE model and CGM method, International J. of Heat and Mass Transfer, (2009)52: 2714-2720.[4]Liu H. C., Wang J. H., Numerical Investigation on Synthetical Performances of Fluid Flow and Heat Transfer of Semiattached Rib-channels,International J. of Heat and Mass Transfer, (2010)53:[5] Wang J. H., Gan M., Detecting and Characterization of Penetrating Pores of Porous Materials, Materials Characterization, 58(2007)8-12.[6] Shi J. X., Wang J. H., Optimized Structure of Two Layered Porous Media with Genetic Algorithm for Transpiration Cooling, International J. of Thermal Science, (2008)47:1595 -1601.[7] Shi J. X., Wang J. H., Inverse problem of estimating space and time dependent hot surface heat flux in transient transpiration cooling process, International J. of Thermal Science, (2009)48:1398-1404[8] Wang J. H., Han X. S., Numerical Investigation of Transpiration and Ablation Cooling, Heat Mass Transfer, (2007)43:274-284.[9] Wang J. H., Wang H. N., Sun J. G., Wang J., Numerical Simulation of Control Ablation by Transpiration Cooling, Heat Mass Transfer, (2007) 43:471-478.[10] Shi J. X., Wang, J. H., A Numerical Investigation on the Laminar Boundary Flow Layer with Transpiration Cooling, Transp Porous Med, 2008. 9, DOI 10.1007/s11242 -008-9279-8.[11] Peng L. M., Wang J. H., Li H., Zhao J. H., He L., Synthesis and Microstructural Characterization of Ti-Al 3 Ti Metal-intermetallic Laminate Composites, Scripta Materialia, 52 (2005) 243-248.[12] Peng L. M., Wang J. H. , Li H., He L., Zhao J. H., Synthesis and Mechanical Properties of Ternary Molybdenum Carbosilicide and Its Composite, J. of Materials Science, 40 (2005) 2705-2707.[13] Peng L.M., Li H., Wang J. H. , Processing and Mechanical Behavior of Laminated Ti- Al 3 Ti Composites, J. of Materials Science and Eng. A 406 (2005)309-318.[14] Wang J. H., Messner J., Stetter H., An Experimental Investigation of Transpiration Cooling, Part I- An Application Investigation on Infrared Measurement Technique, International J. of Rotating Machinery, April 2003, Vol 9, No. 3, 154-163.[15] Wang J. H., Messner J., Stetter H., An Experimental Investigation of Transpiration Cooling, Part II- Comparison of Cooling Methods and Media, International J. of Rotating Machinery, Aug. 2004,Vol 9, No.10, 355-363.[16] Peng L. M., Li H., Wang J. H., Gong, M., High Strength and High Fracture Toughness Ceramic-iron Aluminid3 (Fe 3 Al) Composites, Materials Letters 60 (2006) 883-887.[17] Peng L. M., Li H., Wang J. H., Gong, M., Synthesis and Microstructural Characterization of Aluminum Borate Whiskers, Ceramics International 32 (2006)365-368.[18] Peng L. M., Wang J. H., Li H., Gong M., Processing and Mechanical Properties of Multiphase Composites Based on Mo-Si-Al-C system, J. of Alloys and Compounds 420(2006) 77-82.[19]贾闪,王晓春,王建华, 具有发散冷却功能的曲目结构边界层特性实验研究,航空动力学报,(2010)第25卷,第2期.[20] 周杰,王建华,气动汽车高压气体减压过程的能量损失与补偿,液压与气动,(2007)第7期,28-32.[21] 谢远远,王建华,发散冷却控制烧蚀过程的数值研究,航空动力学报,(2008)第23卷,第8期.[22] 时骏祥,王建华,发散冷却最小冷却介质注射量的数值研究,航空动力学报,(2007)第22卷,第2期.[23] 马龙,王建华,吴向宇,杜治能,利用红外技术进行层板冷却特性实验研究,航空动力学报,(2007)第23卷,第4期.[24] 孙纪国,王建华,烧结多孔结构的渗透和流阻特性研究,航空动力学报,(2008)第23卷,第1期.[25] 李谦,王建华,吴向宇,杨士杰,冷却介质在层板内流动特性研究,第一部分,利用粒子图像测速技术再现复杂流场,实验流体力学,(2007)第21卷,第4期.[26] 王储,王建华,杜治能,杨士杰,冷却介质在层板内流动特性研究,第二部分,数值模拟复杂结构内流场,实验流体力学,(2007)第21卷,第4期. [1]Wang J. H.,Liu Y. L., Wang X. C., Du Z. N., Yang S.J., Characteristics of Tip Leakage of the Turbine Blade with Cutback Squealer and Coolant Injection, Proc. of ASME Turbo Expo 2010 Power for Land, Sea, and Air, June 14-18, 2010, Glasgow, UK, GT2010-22566.[2]Wang J. H.,Liu H. C., Mao M., Li X., Zhang Z. Q., Numerical Investigation of Fluid Flow and Heat Transfer Performances of Semiattached Rib Channel Design, Proc. of ASME Turbo Expo 2010 Power for Land, Sea, and Air, June 14-18, 2010, Glasgow, UK, GT2010-22563.[3]Zhang H., Wang J. H., Wu X. Y., Lu H. Y., A Simplified Approach to Design Transverse Ribs Which Array Alternately in Rectangular Channel,Proc. of ASME Turbo Expo 2010 Power for Land, Sea, and Air, June 14-18, 2010, Glasgow, UK, GT2010-22562.[4] Wang J. H., Lv X. J., Liu Q.D., Wu X. Y., An Experimental Investigation on Cooling Performance of a Laminated Configuration Using Infrared Thermal Image Technique, Proc. of ASME Turbo Expo 2008 Power for Land, Sea, and Air, June 8-12, 2009, Orlando, Florida, USA, GT2009-59838.[5] Wang J. H., Xu H. Z., Lv X. J., Du Z. N., Yang S. J., A Nnmerical Investigation on Fluid-Thermal- Structure Coupling Characteristics of Laminated Film Cooling Configurations, Proc. of ASME Turbo Expo 2008 Power for Land, Sea, and Air, June 8-12, 2009, Orlando, Florida, USA, GT2009-59604.[6] Wang, J. H., Xu, H. Z., Liu, Y. L., Du, Z. N., Yang, S. J., Experimental and Numerical Investigations on Turbine Airfoil Cooling Designs, Part I-An Investigation on Flow Features by Particle Image Velocimetry, Proc. of ASME Turbo Expo 2008 Power for Land, Sea, and Air, June 14-17, 2008, Berlin, Germany, GT2008-50673.[7] Wang, J. H., Xu, H. Z., Liu, Y. L., Wu, X. Y., Yang, S. J., Experimental and Numerical Investigations on Turbine Airfoil Cooling Designs, Part II-An Investigation on Heat Transfer Features by Infrared Thermal Imaging Technique, Proc. of ASME Turbo Expo 2008 Power for Land, Sea, and Air, June 14-17, 2008, Berlin, Germany, GT2008-50674.[8] Wang, J. H., Messner, J., Casey, V. M., Performance Investigation on Film and Tran- spiration Cooling, Proc. of ASME Turbo Expo 2004 Power for Land, Sea, and Air, 14-17 June 2004, Vienna, Austria,GT2004-54132, ISBN: 0-7917-3739-4.[9] Wang H. N., Wang, J. H., A Numerical Investigation of Ablation and Transpiration Cooling Using the Local Thermal Non-equilibrium Model, Proc. of 42nd AIAA/ASME/ SAE/ASEE Joint Propulsion Conference & Exhibit, 09-12, July, 2006, Sacarmento California, USA 2006-AIAA-5264.[10] Wang, J. H., Messner, J., Stetter, H., An Experimental Investigation of Transpiration Cooling, Part I- An Application Investigation on Infrared Measurement Technique, Proc. ISROMAC-9, 10-14 Feb. 2002, Honolulu, Hawaii, USA.[11] Wang, J. H., Messner, J., Stetter, H., An Experimental Investigation of Transpiration Cooling, Part II- Comparison of Cooling Methods and Media, Proc. ISROMAC-9, 10-14 Feb. 2002, Honolulu, Hawaii, USA.[12] Stetter, H., Wang, J. H., Basic Performance Characteristics of a Transpiration Cooling Method for Turbine Nozzle Guide Vane Using Evaporating Liquids, Proc. of 4th European Conference on Turbomachinery, 20-23 March 2001, Firenze , Italy , ISBN 88-86281-57-9.[13] Stetter, H., Wang, J. H., Messner, J., An Experimental Investigation of Transpiration Cooling, Part I- Feasibility Test and Performance Estimation, Proc. ISROMAC-8, 26-30 March 2000 Honolulu, Hawaii, USA, Vol. 1, pp.778-785, ISBN#0-9652469-9-x.[14] Wang, J. H., Stetter, H., An Experimental Investigation of Transpiration Cooling, Part II- Performance Comparison With Film Cooling, Proc. ISROMAC-8, 26-30 March 2000, Honolulu, Hawaii, USA, Vol. 1, pp.786-792, ISBN#0-9652469-9-x.

航天科工704所的核心期刊有哪些

航空学报、推进技术、宇航学报等。航天科工704所的核心期刊包括航空学报、推进技术、宇航学报等知识。《航空动力学报》期刊影响因子在航空航天类期刊中排名第二。

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