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Online since: December 2012
Authors: X. Yan, G.F. Zhou, C.M. Zhu, J.S. Guan
Wuhan University of Science and Technology, Wuhan 430081, China
2.
Experimental Material and Procedure The as-received steel with a thickness of 12mm was provided by a steelworks.
Key Engineering Materials, 1993,84-85:491-520 [4] DHUA S.K., MUKERJEE D., SARMA D.S.
Metallurgical and Materials Transactions A, 2001.9:2259-2267 [5] Zhao X.Q.
Journal of Iron and Steel Research(International),2007 (supplement):240-244 [6]Yan X., Zhou G.F., Chen W., et al.
Experimental Material and Procedure The as-received steel with a thickness of 12mm was provided by a steelworks.
Key Engineering Materials, 1993,84-85:491-520 [4] DHUA S.K., MUKERJEE D., SARMA D.S.
Metallurgical and Materials Transactions A, 2001.9:2259-2267 [5] Zhao X.Q.
Journal of Iron and Steel Research(International),2007 (supplement):240-244 [6]Yan X., Zhou G.F., Chen W., et al.
Online since: May 2014
Authors: Krit Choeisai, Natthaphon Phokhaphan
Electric current which flows through the resonant capacitor is also large at resonant frequency which may give a result in extremely high voltage stress dielectric materials of the capacitor.
The completed antenna is made by a two layers PCB with FR-4 epoxy material as the insulation-dielectric board that hold both layers together.
Kurs, Power Transfer Through Strongly Coupled Resonances, MIT Master of Science in Physics Thesis, Sep. 2007 [2] J.
Minges, Electronic Material Handbook, Vol. 1;Packaging, ASM International Committee, 1989, pp. 536 [12] S.
Lee, Simple Accurate Expression for Planar Spiral Inductances, IEEE Journal of Solid-State Circuits, vol. 34, no. 10, (1999), 1419-1424
The completed antenna is made by a two layers PCB with FR-4 epoxy material as the insulation-dielectric board that hold both layers together.
Kurs, Power Transfer Through Strongly Coupled Resonances, MIT Master of Science in Physics Thesis, Sep. 2007 [2] J.
Minges, Electronic Material Handbook, Vol. 1;Packaging, ASM International Committee, 1989, pp. 536 [12] S.
Lee, Simple Accurate Expression for Planar Spiral Inductances, IEEE Journal of Solid-State Circuits, vol. 34, no. 10, (1999), 1419-1424
Online since: August 2016
Authors: Priyo Suprobo, Wahyuniarsih Sutrisno, Endah Wahyuni, Data Iranata
Introduction
Concrete is heterogeneous materials which consist of a lot of pores.
Cyclic wetting and drying causes continuous moisture and harmful materials movement through concrete pores.
Science. 69(24) (2013) 97–109
Weyers, Modeling Time to Corrosion Cracking in Chloride Contaminated Reinforced Concrete Structures, ACI Material Journal. 95(6) (1998) 675–681
Cyclic wetting and drying causes continuous moisture and harmful materials movement through concrete pores.
Science. 69(24) (2013) 97–109
Weyers, Modeling Time to Corrosion Cracking in Chloride Contaminated Reinforced Concrete Structures, ACI Material Journal. 95(6) (1998) 675–681
Online since: November 2011
Authors: Run Hua Liu, Gang Wang
Poesio P and Ooms G, “Formation and ultrasonic removal of fouling particle structures in a natural porous material,” Journal of Petroleum Science and Engineering,Italy, vol.45, pp. 159-178, November 2004
He Ning, GAO Song and WANG Jie, “Modulation Method of Cascaded Multilevel Distributed Switching Power” Journal of Xi’an Technological University,China, vol.28, pp. 552-556, 2008.
He Ning, GAO Song and WANG Jie, “Modulation Method of Cascaded Multilevel Distributed Switching Power” Journal of Xi’an Technological University,China, vol.28, pp. 552-556, 2008.
Online since: November 2012
Authors: Yue Sun, Jia Liu, Dong Qiang Xu
In order to analysis the feasibility of cancelling setting invert, 3 kinds of models are set as following:
Model 1: ordinary flat-bottom tunnel model
Model 2: inverted tunnel model
Model 3: flat-bottomed tunnel (Grouting bolts bellow the tunnel and pouring C25 concrete on the bottom tunnel where digs out 20cm-thickness original rock)
Surrounding rock uses HowkBrown models, and the remaining material uses a linear elastic constitutive relation.
Journal of Geotechnical Engineering, 1996, 18 (1): 43 – 461.In Chinese
International Journal of Rock Mechanics and Mining Sciences, 2007, 44( 4) :550-564.
Journal of Geotechnical Engineering, 1996, 18 (1): 43 – 461.In Chinese
International Journal of Rock Mechanics and Mining Sciences, 2007, 44( 4) :550-564.
Online since: July 2011
Authors: Bao Hui Wang, Xue Sun, Hui Li, Ying Chen
Introduction
Solid superacid is a kind of new-type catalyst material, it has shown better applicability in many organic catalysis, such as esterification, acylation, alkylation, isomerization, and so on [1, 2].
[4] Lian Ping, Yang Yanchao.Preparation and characterization for rare earth solid superacids Gd3+-SO42-/ZrO2 catalyst [J].Journal of Gannan Normal University, 2005, (3):50-51
[5] Shen Xiangzhong, Xie Shanmei, Hu Ting.Research of rare earth solid superacids nanometer SO42-/TiO2/La the preparation and catalytic synthesis of allantoin [J].Journal of Hunan Institute of Humanities; Science and Technology, 2008, (2):22-26
[4] Lian Ping, Yang Yanchao.Preparation and characterization for rare earth solid superacids Gd3+-SO42-/ZrO2 catalyst [J].Journal of Gannan Normal University, 2005, (3):50-51
[5] Shen Xiangzhong, Xie Shanmei, Hu Ting.Research of rare earth solid superacids nanometer SO42-/TiO2/La the preparation and catalytic synthesis of allantoin [J].Journal of Hunan Institute of Humanities; Science and Technology, 2008, (2):22-26
Online since: May 2007
Authors: Wei Min Pan, Ji Shun Li, Y. Lei
Lei2,c
1
School of Mechatronics Engineering,Henan University of Science & Technology, LuoYang,
471003,China
2
School of Mechanical Engineering & Automation,Beihang University, Beijing, 100083,China
a
wmpool1@163.com,
b
li_jishun@163.com, cylei@caxa.com
Keyword: CAD, CMM, Digital measure, Spiral bevel gear
Abstract.
Examples of product data are geometry, topology, material, dimensions, tolerance and assembled structure.
Wang: Chinese Journal of Aeronautics, (August 2003), pp.182-186
Murugappan: The International Journal of Advanced Manufacturing Technology, (2000) No.16, pp.107-112
Examples of product data are geometry, topology, material, dimensions, tolerance and assembled structure.
Wang: Chinese Journal of Aeronautics, (August 2003), pp.182-186
Murugappan: The International Journal of Advanced Manufacturing Technology, (2000) No.16, pp.107-112
Online since: January 2012
Authors: Cong Hu, Zhi Jin Qiu, Jun Hao Niu
In the aerospace, aviation, weapons manufacturing, science research, new material development, precision production, storage and other places with strict temperature and humidity requirements, the change of the environmental conditions change will have a direct impact to the performance of the product, or even lead to serious accidents.
Coal Mine Machinery. 2009.30(6). p.20-23 [5] KUANG Yuguo: Application of Intelligent Sensor SHT11 in Portable Warm-Humidity Detector Chinese Journal Of Electron Devices. 2006.29(4). p.1313-1315 [6] TIAN Yongjun, ZHAO Guangqiang, ZENG Jianping: Design of Data Multi-communication Between PC and Single Chip Computer Based on RS485.
Journal of Hunan Institute of Engineering. 2007.17(2). p.19-23
Coal Mine Machinery. 2009.30(6). p.20-23 [5] KUANG Yuguo: Application of Intelligent Sensor SHT11 in Portable Warm-Humidity Detector Chinese Journal Of Electron Devices. 2006.29(4). p.1313-1315 [6] TIAN Yongjun, ZHAO Guangqiang, ZENG Jianping: Design of Data Multi-communication Between PC and Single Chip Computer Based on RS485.
Journal of Hunan Institute of Engineering. 2007.17(2). p.19-23
Online since: June 2008
Authors: Claude Bathias, Hua Tao, Sen Ge, Chuang Shao
According to this way, we had also gotten the
dynamic S-N curves of varied joint of structure or material and compared the dynamic fatigue
capability of varied stiffener in the test.
Table2 Strain and failure time Specimen number Strain (µε) Loading (grms) Cycle(N ) 1 1172.72 20 1.33E06 2 1173.28 25.5 1.26E06 3 1189.71 20 1.26E06 4 1210.92 25.5 1.20E06 5 1343.35 20 1.11E06 6 1411.49 23.1 1.16E06 7 1468.27 23.1 9.46E05 8 1608.67 23.1 8.16E05 9 1629.29 23.1 7.42E05 10 1671.77 23.1 7.79E05 11 1788.35 25.5 6.30E05 12 1930.13 23.1 7.23E05 13 2010.41 23.1 6.64E05 14 2031.33 23.1 7.16E05 15 2235.61 23.1 6.49E05 16 2301.42 20 5.56E05 17 2435.08 20 5.93E05 18 2624.37 23.1 5.19E05 19 3361.68 23.1 5.01E05 20 3946.35 20 4.63E05 21 3961.29 25.5 4.01E05 22 4132.39 23.1 4.45E05 23 4967.28 25.5 3.34E05 24 5124.29 25.5 2.78E05 5.4 5.5 5.6 5.7 5.8 5.9 6.0 6.1 6.2 2.5 2.6 2.7 2.8 2.9 3.0 3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0 lg¦Årms(¦Ì¦Å) cycle(lgN) Fig.6: εrms-N curve Acknowledgment The author thanks the colleagues of ASRI and this project supported by the fund of aeronautics science and technique
References [1] SHAO Chuang: The Estimate Method of Sonic Fatigue for laminated Panel, Thesis of Master Degree of Northwestern Polytechnical University (2005) (in Chinese) [2] GE Sen, CAO Qi, SHAO Chuang, GUO Dingwen: ACTA Aeronautic et Astronautic SINICA Vol.18 (1997) [3] YAO Qihang: The analects for sonic fatigue of aircraft structure (Aeronautic Industry Press, Beijing 1991) [4] ZHANG A-zhou, ZHANG Kerong, YAO Qihang: Vibration Environment Engineering (Aeronautic Industry Press, Beijing 1986) [5] M.J.Jacobson: Design and Sonic Fatigue Characteristics: Advanced Composite Joints, AFFDL-TR-71-126 (1971) [6] YAO Qihang, YAO Jun: Chinese Journal of Applied Mechanics Vol.23 (2006) [7] SHAO Chuang, GE Sen: Journal of Vibration Engineering, Vol.19 (2006) [8] SHAO Chuang, GE Sen: The research on sonic fatigue characteristic of composite laminated panel (in Chinese), Structural Strength Research, Supplement, (2005)
Table2 Strain and failure time Specimen number Strain (µε) Loading (grms) Cycle(N ) 1 1172.72 20 1.33E06 2 1173.28 25.5 1.26E06 3 1189.71 20 1.26E06 4 1210.92 25.5 1.20E06 5 1343.35 20 1.11E06 6 1411.49 23.1 1.16E06 7 1468.27 23.1 9.46E05 8 1608.67 23.1 8.16E05 9 1629.29 23.1 7.42E05 10 1671.77 23.1 7.79E05 11 1788.35 25.5 6.30E05 12 1930.13 23.1 7.23E05 13 2010.41 23.1 6.64E05 14 2031.33 23.1 7.16E05 15 2235.61 23.1 6.49E05 16 2301.42 20 5.56E05 17 2435.08 20 5.93E05 18 2624.37 23.1 5.19E05 19 3361.68 23.1 5.01E05 20 3946.35 20 4.63E05 21 3961.29 25.5 4.01E05 22 4132.39 23.1 4.45E05 23 4967.28 25.5 3.34E05 24 5124.29 25.5 2.78E05 5.4 5.5 5.6 5.7 5.8 5.9 6.0 6.1 6.2 2.5 2.6 2.7 2.8 2.9 3.0 3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0 lg¦Årms(¦Ì¦Å) cycle(lgN) Fig.6: εrms-N curve Acknowledgment The author thanks the colleagues of ASRI and this project supported by the fund of aeronautics science and technique
References [1] SHAO Chuang: The Estimate Method of Sonic Fatigue for laminated Panel, Thesis of Master Degree of Northwestern Polytechnical University (2005) (in Chinese) [2] GE Sen, CAO Qi, SHAO Chuang, GUO Dingwen: ACTA Aeronautic et Astronautic SINICA Vol.18 (1997) [3] YAO Qihang: The analects for sonic fatigue of aircraft structure (Aeronautic Industry Press, Beijing 1991) [4] ZHANG A-zhou, ZHANG Kerong, YAO Qihang: Vibration Environment Engineering (Aeronautic Industry Press, Beijing 1986) [5] M.J.Jacobson: Design and Sonic Fatigue Characteristics: Advanced Composite Joints, AFFDL-TR-71-126 (1971) [6] YAO Qihang, YAO Jun: Chinese Journal of Applied Mechanics Vol.23 (2006) [7] SHAO Chuang, GE Sen: Journal of Vibration Engineering, Vol.19 (2006) [8] SHAO Chuang, GE Sen: The research on sonic fatigue characteristic of composite laminated panel (in Chinese), Structural Strength Research, Supplement, (2005)
Online since: October 2011
Authors: Yuee Chen, Nan Xiang Chen, Qing Wu
(1) The scientific principle: indexes selected is based on science, shoud have clear concept, and reflects the object's essence
The material sequence was six years from 2002 to 2007.
Journal of Chinese desert (2005)
Review of The Beijing-Tianjin Sandstorm Source Control Engineering Benefit Evaluation Research [J].Journal of Chinese Forestry Industry (2006)
The material sequence was six years from 2002 to 2007.
Journal of Chinese desert (2005)
Review of The Beijing-Tianjin Sandstorm Source Control Engineering Benefit Evaluation Research [J].Journal of Chinese Forestry Industry (2006)