LAMINATES

作品数:142被引量:155H指数:5
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相关机构:南京航空航天大学江西理工大学浙江三维橡胶制品股份有限公司上海交通大学更多>>
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  • 期刊=Transactions of Nanjing University of Aeronautics and Astronauticsx
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Analysis and Control of Surface Delamination Defects During Milling of Orthogonal Aramid Fiber‑Reinforced Composites Laminates被引量:2
《Transactions of Nanjing University of Aeronautics and Astronautics》2020年第3期353-359,共7页SHI Zhenyu DUAN Ningmin LI Xin WANG Zhaohui 
supported by the National Natural Science Foundation of China(No.51975334);Key R&D Project of Shandong Province(No.2019JMRH0407);the Fundamental Research Funds of Shandong University Grant。
The aramid fiber-reinforced composites(AFRC)can increase the durability of corresponding applications such as aerospace,automobile and other large structural parts,due to the improvement in hardness,heat build-up,wear...
关键词:aramid fiber-reinforced composites(AFRC) milling process delamination defects surface control prediction model 
Methods for Reducing Interface Aperture Inconsistency During NC Orbital Milling of Aircraft Laminates with Coarse Pitch
《Transactions of Nanjing University of Aeronautics and Astronautics》2020年第3期446-459,共14页SHAN Yicai HE Ning LI Liang WU Kai 
Natural Science Research in Jiangsu Province(No.17KJB460008);the 333 Project Research Funding Project in Jiangsu Province(No.BRA2018310);the Innovation Project of Jiangsu Province.
The methods for reducing interface aperture inconsistency are studied in NC orbital milling(NCOM)of CFRP/Ti6Al4V laminates with coarse pitch.Comparative experiments show burr,aperture inconsistency and error are typic...
关键词:CFRP/Ti6Al4V laminates NC orbital milling coarse pitch feed interface aperture 
Damage Detection and Material Property Reconstruction of Composite Laminates Using Laser Ultrasonic Technique被引量:4
《Transactions of Nanjing University of Aeronautics and Astronautics》2019年第1期1-16,共16页QIU Jinhao TAO Chongcong JI Hongli ZHANG Chao ZHAO Jinling 
partially supported by the National Natural Science Foundation of China (Nos. 51875277,51805261);the State Key Laboratory of Mechanics and Control of Mechanical Structures(Nanjing University of Aeronautics and astronautics)(No. MCMS-I0518K01)
Laser ultrasonic technique has received increasing attentions in the past decade due to its contactless nature and a wide range of applications have been reported. In this review,applications of laser ultrasonic techn...
关键词:laser ULTRASONIC COMPOSITE LAMINATES DAMAGE detection STIFFNESS RECONSTRUCTION 
Effect of Thermal Treatment on CFRP Parts Before and After Adhesive Bonding被引量:1
《Transactions of Nanjing University of Aeronautics and Astronautics》2018年第2期256-263,共8页Pawe H Malinowski Mirosaw Sawczak Tomasz Wandowski Wiesaw M Ostachowicz 
supported by the European Union's Horizon 2020 Research and Innovation Program (No. 636494)
Numerous non-destructive techniques are being investigated for assuring quality of the adhesive bonds.The research presented here is focused on non-destructive assessment of carbon fibre reinforced polymer(CFRP)parts....
关键词:ADHESIVE joints carbon fibre reinforced polymer (FRP) COMPOSITE LAMINATES COMPOSITE materials andrepairs composites ELECTROMECHANICAL impedance NON-DESTRUCTIVE testing (NDT) 
FATIGUE LIFE PREDICTION METHOD FOR IMPACTED LAMINATES
《Transactions of Nanjing University of Aeronautics and Astronautics》2011年第1期87-93,共7页徐颖 温卫东 崔海涛 
The existing models are established based on the fatigue behavior of impacted laminates.It makes them unsuitable for the general use.So,a general 3-D progressive damage fatigue life prediction method for impacted lami...
关键词:laminated composites fatigue testing IMPACT progressive damage 
INTERLAMINAR FRACTURE TOUGHNESS OF MULTI-DIRECTIONAL LAMINATES
《Transactions of Nanjing University of Aeronautics and Astronautics》2001年第2期176-181,共6页李勇 李顺林 陶杰 
Based on the conventional compliance and area methods, a high precision method named the angle method is presented in this work. The interlaminar fracture toughness is determined by measurement of the load and the ben...
关键词:COMPOSITE LAMINATE DELAMINATION fracture toughness 
A FATIGUE FAILURE CRITERION OF NOTCHED GFRP LAMINATES
《Transactions of Nanjing University of Aeronautics and Astronautics》1999年第2期137-140,共4页夏道家 徐惠民 
A fatigue failure criterion for predicting the fatigue life of notched orthotropic fiber reinforced plasties (FRP) plates based on the concept of stress field intensity (SFI) near the notch root is subjected to furt...
关键词:fatigue damage glass fiber  reinforced plastics laminates notched specimens stress field intensity 
RELAXATION BEHAVIOUR OF GFRP UNIDIRECTIONAL LAMINATES 被引量:3
《Transactions of Nanjing University of Aeronautics and Astronautics》1999年第2期148-153,共6页顾怡 
In this paper two set of GFRP specimens are manufactured and tested to investigate the relaxation behaviour under cyclic loading in the longitudinal and transversel direction. The relaxation of GFRP unidirectional la...
关键词:GFRP RELAXATION FATIGUE unidirectional laminate 
THEORETICAL AND EXPERIMENTAL STUDY ON THE PIEZOCERAMIC ACTUATING LAMINATE
《Transactions of Nanjing University of Aeronautics and Astronautics》1997年第1期90-97,共8页万建国 陶宝祺 朱纪军 
国家自然科学基金;航空科学基金
Piezoelectric ceramic element (PCE) is a kind of actuator applied widely on the intelligent material & structure. Establishing the relationship between the transferring stress and the controlling signal, namely the t...
关键词:piezoelectric  ceramics LAMINATES actuate transfer affecting  factors 
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