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102-105TUltrasonic cutting of individual silver nanowires by a linearly vibrating micro tool se(f[),Op 67-69uAnti-plane problems of a piezoelectric inclusion with an elliptic hole or a crack in an infinite piezoelectric matrix hgwmuQ(f[),ؚX[lؚX[l p 353-358SA two-dimensional study of an elliptic piezoelectric plate compressed diametrically Ngl(f[),ؚX[l p 295-2987A Langevin type piezoelectric tracked travelling systemb g(f[),sN(f[),ё[ci, _^ё[cip 89-93MA tracked travelling system under the actuation of a piezoelectric transducersN(f[),b g(f[),ё[ci, _^p 94-98EThe research on a novel linear stepping piezoelectric stacks actuatorz*mi(f[),sN(f[),ё[ci p 247-250tFinite element formulations and algorithms for coupled multiphysics analysis of 0-1 and 0-3 polarized PLZT actuatorsѐNpg,NzR(Y),Luo, Quantian(Y)ѐNpg?International Journal of Applied Electromagnetics and Mechanicsv 49,n 4,p 513-530:Phonon Trapping in Pearl-Necklace-Shaped Silicon Nanowires*%f m(f[),SV[,hT^e,NgNgSmallv 11,n 48,p 6411-6415Journal of Applied Physics:gh6R NꁨRS&^Scv~|kSfwݍʑ>e[xvz sRb(f[),ё hs^ё hs^RRf[Nc6Rf[bYOĖ^ X6qB\AmWĞwpg(f[),)Y*,fwm~g)Y*]Zhongguo Dianji Gongcheng Xuebao/Proceedings of the Chinese Society of Electrical Engineering 'YW~gKmpOSNMn 4bQ.^(f[),~V[~V[jVXN/cRc6Rޘ:g5u QdQ|~\PleVl/cSpeq_Tĉ_xvzcQNS,hgkSNcQNS*zzyf[b/g -NVl*ޘLf[bf[bؚ5uxmAmhKm|~S[xvz*Ys^(f[),؈ۏim, zQ(f[),c[[=N,m_ONS(f[)؈ۏimVY5uP[Kmϑb/g_\WFd~hhlRyr'`pe\elv'YWΘR:gR`T^T>\xvzf]NS(f[),s TIQ,gNXs TIQsComputational research on aerodynamic characteristics of helicopter main-rotor/tail-rotor/vertical-tail interaction S(f[),_VNS,SRpg_VNSv 36,n 9,p 2874-2883<Ground effect test of tri tilt-rotor aircraft in wind tunnelHdW(f[),S_O,Y[RN(f[)v 36,n 9,p 2884-2891{Self-powered synchronized switch damping on negative capacitance for broadband vibration suppression of flexible structures.Qureshi, Ehtesham Mustafa(f[),lf,Chang, Lulu(f[)v 49,n 1,p 105-121SSWR`1YlR!jWxvz \=NZ(f[),YTGYYTGYu8l_](f[),sz\,~Q(f[)gFinite element analysis of strain 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under Earth's gravity and hypergravity&e$_,Li, Guohua(f[),Li, Dingkun(f[),s(f[)/International Journal of Heat and Mass Transferv 87,p 399-408ZEffects of nonlinearity on transient processes in AT-cut quartz thickness-shear resonatorsNg_(f[),_NS,hg V[(Y)Acta Mechanica Solida Sinicav 28,n 4,p 347-352\Extension of concurrent subspace optimization to structural optimization of product familiesT(f[),YkSf,Y)Y(f[)-Structural and Multidisciplinary Optimizationv 52,n 2,p 281-291LSynergistic damage evolving model for matrix cracking in composite laminateslimpg(f[),YkSf,4TIN(f[)v 32,n 4,p 1032-1041bOn the initial function space of time-delayed systems: A time-delayed feedback control perspective s`x,HsQc(Y)!Journal of the Franklin Institutev 352,n 8,p 3243-3249bFinite element analysis of crack propagation paths and crack initiation loads in graded compositesLyu, Yi(f[), ^fk,heyv 32,n 4,p 1099-1106 s^^(f[),RHQeRHQePhysica Scripta v 90,n 8,VAn ultrasonic manipulator with noncontact and contact-type nanowire trapping functions v 232,p 13-19WWind-induced fatigue analysis of wind turbine system based on tower-blade coupled modelv 32,n 8,p 36-41NHybrid grid DSMC method for chemical nonequilibrium with rarefied flow heating H\ z(f[),s_l\v 32,n 4,p 408-414sInfluence of geometry of composite cruciform specimen under biaxial loading on coefficients of central testing zone!{v[(f[),hTIQf,f6q(f[),s!hW(f[)v 32,n 4,p 1138-1144EExperiments on an open-loop cycle carbon dioxide refrigeration system_(f[),f_,ѐ\*o(f[),!sޘ(f[)v 32,n 4,p 452-460.Advance in electrokinetic phenomena and theoryNg,Fei, Wenwen ,(f[)v 35,n 4,p 603-612wPower extraction efficiency improvement of a fully-activated flapping foil: With the help of an auxiliary rotating foil4Tpg,ysOnf(f[),sf(Y),u[ Journal of Fluids and Structuresv 57,p 219-228WNWENO͑gveWeQ3 nanoparticles from K2Ti6O13 precursors!f m(f[),1gT[Q,Du, Jianzhou(f[),RR~g,؈ۏimv 41,n 7,p 4851-4859?s(f[),S_O, zKQf,1g~v(f[)hNumerical simulation and experimental research of a flexible caudal fin by piezoelectric fiber composite+[ng(f[),NgNS\,Yang, Xi-Xin(f[),Peng, Han-Min(f[)NgNS\"ADVANCES IN MECHANICAL ENGINEERING wS: 7 g: 7Ng*mS,Ma, Yuan-Zhuo(f[)]Open/Closed-Loop Aeroservoelastic Predictions via Nonlinear, Reduced-Order Aerodynamic ModelsĞ,Ng?dW(f[),wm\,u8l AIAA JOURNALwS: 53 g: 7 u: 1812-1824kInfluence of a flexible tail on the performance of a foil hovering near the ground: Numerical investigation4Tpg,Rt(f[),hgm(f[),u['European Journal of Mechanics, B/Fluids v 52,p 85-96WNSpeS gPCQelv:g͑ϑKmk _e(f[),[(f[),'k3f(f[),YOĖ^ l(uޘ:gNxvz{:gR] zCMeasurement: Journal of the International Measurement ConfederationZModeling and sticking motion analysis of a vibro-impact system in linear ultrasonic motorsNgT(f[),Y_܏,Wu, Ranchao(f[) v 100,p 23-31WN9eۏvEMDelTϑ{P[lvnEeʋe pg(f[),~V[lt]'Yf[f[b(6qyf[Hr)Ahg~g^@\OSvv^LP[zzel sk(f[),YkSf] zf[bFShanghai Jiaotong Daxue Xuebao/Journal of Shanghai Jiaotong UniversityO}[wb_SQ4lAmRyr'`q_Tv[xvzNgQ(f[),[O, _(f[),s*m(f[) 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Ng_(f[),HnfOv 47,n 3,p 458-470RExperimental verification of chaotic attitude motion of tethered spacecraft system ^FQT(f[),ё hs^v 47,n 3,p 503-512CMicromorphic model of graphene-like two-dimensional atomic crystalshgR(f[), _ev 47,n 3,p 451-457 YTPgeB\TgS)}w Nnۏ_c$ORgNՋ1g^(f[),f^_l,Hn&t(f[),zfl ؚO(f[),c[[=N,؈ۏimc[[=NWDesign and characteristics analysis of hybrid isolator based on laminated PVDF actuatorv 34,n 9,p 141-148{g(f[),Y_܏,hg!j\(f[),R/c(f[)A general and simple method to synthesize well-crystallized nanostructured vanadium oxides for high performance Li-ion batteries+Ng=NS(f[),Liu, Pengcheng ,(f[),1gT[Q,sleN,RR~g,؈ۏimv 3,n 18,p 9385-9389ޘ:gzzl[{loyr'`vՋxvzSpex(f[),NgO(f[)v 30,n 5,p 1267-1274@Structure design of beam type clamp for V-shape ultrasonic motorv 23,n 5,p 1358-1364\A switching median-mean filter for removal of high-density impulse noise from digital imagesv 126,n 9-10,p 956-961RResearch on safety analysis for airborne system based on extended functional model.l(f[),1g%fs,Cao, Dejian(f[),Huang, Chuanlin(f[),"eP wS: 7 g: 5%NR,Y[im(Y),Haim Waisman(Y)%NR{A guided Bayesian inference approach in structures using the extended finite for detection of multiple flaws element methodCOMPUTERS & STRUCTURESwS: 152 u: 27-44jInfluence of regenerator void volume on performance of a precooled 4 K Stirling type pulse tube cryocooler NgSS,f_,HpgNgSS Cryogenics v 70,p 34-40dDesign of active flutter suppression and wind-tunnel tests of a wing model involving a control delayĞ,eOe(f[),wm\,u8lv 55,p 409-427R717{QAmRl~ OpsQ|_ċNRgs f(f[),e$_,sm(f[),l%f(f[)AmSO:ghLCreep effect analysis at the friction interface of a rotary ultrasonic motorH,XO]lv 7,n 2,YeQYQck&_kbՋc6Reel _ekN(f[),H`wm,:eNiMicromechanical analysis of SiC/Al metal matrix composites: Finite element modeling and damage simulationSwm,Liu, Tianliang(f[)SwmgMulti-modal optimal fuzzy active vibration control of a photo-electric laminated simply supported plate :[l(f[),ѐNpgv 34,n 8,p 77-82 and 116TStall flutter computation of turbomachinery blade based on a CFD/CSD coupl< ing methodhT(f[),F_o, T^,li``i(f[)v 36,n 4,p 1076-1085Aeroelasticity of helicoptersof,Chen, Quanlong(f[),XTwmsofv 36,n 4,p 1034-1055 O|~~TޘL'`Rg H^s^, _~,zflWN5uSf[Plvc6RYxvzY[[T(f[),؈ۏim,c[[=N,1gT[Q,H܏_f(f[)^(uS]~g/cRuRՋvKmelxvz ~SfNS(f[),H`wmWNCFD|~Ƌvl9_RgSGPUv^L{lRc Ğp(f[),u8lWNADAMSv^9YcirSOqRxvzROeP(f[),Y[_\, _l(f[)L]eQ_X5u:g_ekݍc6RhKm|~ ѐKN(f[),Y[_\Jun, Li(f[),ؚWO,Hong-Wei, Liu(f[)Open Civil Engineering Journal 9120-124WNёfcKm:ghU\__ۏeQޘLhVb/gċNgeN(f[),\fS(f[), _~,zflqQtSe`\P0WbHe^lRyr'`RgqNS(f[),1gnNS,~g(f[)Ny(uNvGS:gi_vޘLRf[RgelBhleQ(f[),HNo,Nge,T[kS~vGS:gsϑc6R>\h*bbb_rRg Ng[%f(f[),hgkSN5uce OahV|~YO^ShQ{lxvz sR`V(f[),F m hT(f[),of:g^_T[0}vGS:g@w0WAm:Wvq_Txvz Ğe(f[),_VNS,SRpg\Vibration fatigue life prediction method for structures under multi-axial random excitationsv 34,n 7,p 59-63Ǐ!nr`>PlelRR!jbvؚHeCFDelNgO(f[),b/TQ,jlck-N(Y),sZSWNCEMelvvGS:gRCS{SSpeRg_[hf(f[),b/TQ,v(f[)V~eޘLhVv N~~gSЏRL]WYQN(f[),eЏeg,umueЏegPsX Nk_{huRՋeHhxvz SfN(f[), _QR,*mm(Y),ؚ\ n(Y),~Q,Sf(Y);Optimization-driven design method of landing gear structure" _f,Liu, Wenbin(f[),Li, Chuang(f[),B[v 36,n 3,p 857-864lEnergy harvesting performance of a dandelion-like multi-directional piezoelectric vibration energy harvester)HNe,N(f[),Yfh^(f[),tQfk(f[),Liu, Xiangjian(f[) v 230,p 1-8OEquivalent multi-case optimization architecture for modular aircraft structures _z0N(f[),YkSf,T(f[)v 36,n 3,p 834-839BProportional control of jet deflection with passive secondary flow@f8lޘi(f[),~t~g, zKQf,Xiao, Zhongyun(Y),Chen, Zuobin(f[),He, Kaifeng(f[)v 36,n 3,p 757-763DA phenomenological constitutive model for shape memory polyurethanes~^s^(f[),Y[gas,e8^R(f[)v 26,n 5,p 517-526l~gkހr~gvUSހbQI{He!jϑRgSvQq_TV }Ngpg (f[),lf,Hёё(f[)ؚXXgAmVp&T^!jNRg hgfk(f[),ofvW]f[bf[b(6qyf[Hr)Y:W&Tv:gplR9_'`xvz _ޘ(f[),ofTPrediction of separation shock environment based on genetic algorithm and BP network [[Y(f[),Sl[cProceedings - 2014 7th International Symposium on Computational Intelligence and Design, ISCID 2014 v 1,p 453-456 ETC|~xQc!jWxvzd(f[),^IQ,YOePVf(f[),O}v(f[)-NVNOo`SuV^(f[),b/TQ,4T*t(f[)dExperimental investigation of synthetic jet control on large flow separation of airfoil during stall!uV^(f[),b/TQ,~t~g,H ^(f[), _Q(f[),]O(f[)v 47,n 2,p 351-355L]eQ_'Ylpenc|~Kriging{l!jWs8e,Rf[:_,[,k(f[)Novel electromagnetic modeling approach of carbon fiber-reinforced polymer laminate for calculation of eddy currents and eddy current testing signals: zQ(f[),c[[=N,؈ۏim,Takagi, Toshiyuki(f[),Uchimoto, Tetsuya(f[),1g[v 49,n 5,p 617-631`Improvement of mass conservation and reduction of spurious oscillations for the local DFD method _lb(f[),hT%fNS,~O:_(Y)5International Journal of Computational Fluid Dynamicsv 29,n 3-5,p 257-271xAeroelastic analysis of helicopter rotors using computational fluid dynamics/comprehensive analysis loose coupling model [(f[),_VNS,SRpgv 229,n 4,p 621-630 YTPge~T9_'`!jϑuRpQĉ_xvz hg[U(f[),4T[:_4T[:_  YTPge)Y~iYf[yOSTNs(f[),hTIQf,ROHQ(f[)zzzg'`*Y3pS/cRRg T[ey[(f[),s_~t< 1Sound energy harvesting using an acoustic grating v 117,n 10, l xmQWegbˆ'`xvz!u?e(f[),ؚWO,sNSO(Y),?ޘ,R[O(f[),YhCQ(f[)4lRS5u]Two-dimensional near-field multiple signal classification algorithm-based impact localizationNa,N8l~(f[),,s_Q(f[)v 26,n 4,p 400-413XA dynamic compensation system of passive controllable reactor for piezoelectric actuator"NgNS\,Li, Sunan(f[),Zhang, Benfeng(f[)v 35,n 5,p 1237-1242 N8l~(f[),Na,(Structure and Infrastructure Engineeringv 11,n 3,p 310-320>Two-Dimensional Problem of a Crack in Thermoelectric Materials[jO,ؚX[l,Ng_l[(Y)Journal of Thermal Stressesv 38,n 3,p 325-337Ǒ(uI{He gPCQ!jWv YTPge:g~gOS s[,'k3f(f[),YOĖ^WUltraviolet or atomic irradiation effect on the polyimide composite lubricating coatinguv,N^Q,sPNS(Y),m_peJournal of Polymer Engineeringv 35,n 2,p 145-150VCorotational nonlinear dynamic analysis of thin-shell structures with finite rotationshgR~g,YTGY AIAA Journalv 53,n 3,p 663-677Y[N3(f[),HVs^,elb(f[),sW(f[),Y[]lpg(f[)Mechanism and Machine Theoryv 85,p 106-115kA universal moving-embedded grid method for CFD simulation of unsteady aerodynamic characteristics of rotorv 30,n 3,p 546-554JDesign of diamond piezoelectric micro displacement amplification mechanismĞkSn,S\^(f[),s[(Y)v 23,n 3,p 803-809qMonitoring of crack propagation in repaired structures based on characteristics of FBG sensors reflecting spectraNa,ёk(f[),,Huang, Hong-Mei(f[)BGuang Pu Xue Yu Guang Pu Fen Xi/Spectroscopy and Spectral Analysisv 35,n 3,p 724-729zFinite element analysis and experimental research on mechanical performance of bolt connections of corrugated steel platesUbe,9\Q\(Y),\f(Y),]of(Y)Ube)International Journal of Steel Structuresv 15,n 1,p 193-204]The influence of particle shapes on strength and damage properties of metal matrix compositesv 15,n 8,p 5741-5748LSet-membership Identification Method for Helicopter Flight Dynamics Modeling4TO,HNo4TOJournal of AircraftVol.52 No.2 p553-560xInfluence of ventilation rate on the aerodynamic interference between two extra-large indirect dry cooling towers by CFDgNX,hO(Y),ug(Y),[T(Y)-Wind and Structures, An International Journalv 20,n 3,p 449-468PNumerical simulation of compressible flows based on hybrid Cartesian grid methodl_O(f[),u[,Hu, Ou(f[)v 30,n 3,p 513-525SjR YTPgeRK{s^gK{ageRyRgNgV_(f[),zfl,1gfNNS:ggbhrc4YTSpeOS 4TN(f[),YkSfё^\RK{gS)3z['`Rgv:g:wl NgQ#(f[),Ube,zflV{/elx9Y_9YB\fgv1u/cR ^R(f[),[}vlDesign and analysis of a zero Poisson's ratio mixed cruciform honeycomb and its application in flexible skin zepg(f[),hT=N, _s^(f[),m(Y)v 36,n 2,p 680-690WNABAQUSvΘR:gte:g gPCQ^!jTRRRghO(f[),slfk,Xoeh(f[),O(f[)slfk5uRf[bPBXpo|9_'`_c$O,gg!jWSpeOea^Rg ؚQ(f[),ĞQtQQu|ev:gyr'`SR~elxvz4T~t,1gx(f[),of[*(f[)$Mathematical Problems in Engineeringv 2015,YA Bayesian approach for localization of acoustic emission source in plate-like structures%NR,dlQRޘޘ:gzzl[{-Nv/_{^Ryr'`xvz 4Tb(f[),ʃybNRe:g5uRp2QRpRsR^OSxvz1gIQN(f[),Ngc V(f[), _'Yg _'YgWNDTSvno[ϑvKmSL'`Ջxvz#ue,hTR(f[),hTguQ(Y),4TR(Y)," (Y),YQR(Y) 4l5uꁨRSN'Y]WvKmޘ:gsc|~_ld\hVNwxvz Ğckw(f[),H~^H~^ gWޘ:g^1pRg  _f_(f[),H~^{:g] zNeWeQAeroelastic simulations of a large horizontal-axis wind tubinev 28,n 1,p 38-43OOrder selection for wavelet series decomposition in dynamic load identificationv 35,n 1,p 56-62dA multi-branch finite deformation constitutive model for a shape memory polymer based syntactic foam v 24,n 2,Effect of Time Delay and Cross-Correlated Noises on Stochastic Resonance for a Metapopulation System with a Multiplicative Periodic Signal wS: 53 g: 1Hss(f[),e$_,s(f[),ςTAnnals of Nuclear Energyv 76,p 451-460VMeasurement of pore water pressure in asphalt pavement and its effects on permeabilityؚO/T,bb(f[),Rsm(f[) v 62,p 81-87hAnalysis on wind-induced responses of large wind power structures considering soil-structure interactiongNX,s TIQ,f]NS(Y),ug(Y),[T(Y)5Tumu Gongcheng Xuebao/China Civil Engineering Journalv 48,n 2,p 18-25Effect of the stiffener stiffness on the buckling and post-buckling behavior of stiffened composite panels - Experimental investigation1gfNNS,Yan, Jiayi(f[),Hzf(f[),zfl,sÍhQv 120,p 334-3456Vibration de-icing method with piezoelectric actuators}v)Y(f[),1g%fs,ׂl(f[),NgQ(f[),1g zwS: 17 g: 1 u: 61-73UDevelopment and validation of a new two-dimensional wake model for wind turbine wakesu[,Shen, Zhiwei(f[)7Journal of Wind Engineering and Industrial Aerodynamics v 137,p 90-99IContact and friction behavior of piezoelectric vibrator for driving trackĞ(f[),sN(f[),b g(f[),z*mi(f[),ё[civ 35,n 1,p 170-177>Dynamic analysis of a high-speed flexible parallel manipulator _l(f[),hT=Ns^(f[),ё[ci, _^v 28,n 1,p 27-37HManoeuvres o< f spacecraft with flexible appendage in obstacle environment4T\eP(f[),eim,Hc(f[)eim6International Journal of Space Science and EngineeringVol.3, No.1, p.16-30OResearch of elastic modulus for vibration behavior of flexible bionic fish tail%[ng(f[),NgNS\,Yang, Xixin(f[),Di, Sisi(f[)v 35,n 1,p 12-169eۏWeS|P[(WVPMQ-Nv^(u1g(f[),HNe,zؘs(f[)uEffect of thickness on the stress and magnetoelectric coupling in bilayered Pb(Zr 0.52 Ti 0.48 )O 3 -CoFe 2 O 4 filmssgZ,Ng\(f[),s^Q(f[),UOlPg(f[),WSV{e(f[)sgZ v 117,n 4,gWind-induced response analysis of wind turbine tower considering rotationaland centrifugal force effectv 36,n 1,p 33-40ceWPgemQW!niegbˆ'`xvz&Hl f(f[),ؚWO, OkS(Y), _fNw(Y),_\N(f[),TO(f[)lStrain tunable electronic and magnetic properties of pristine and semihydrogenated hexagonal boron phosphide Nۏ(f[),Ng v 106,n 4,ؚޘLhVzzT RSR;NRc6RN^~'`pe?@>G=>AB=0O ?@>5:B8@>2>G=0O <>45;L B>=:>AB5==KE :>=AB@C:F89 s_~t,^(f[)5AB=8: "#. !1sX{|WN/lvSm^[w#nmQWhb/lyP[Sm^vq_T$kS(f[),YO~S,zf"(f[),wm0(f[),\(f[),l(f[)RpeMO[AmRl~4NLupAm[^q_TNgQ(f[),[O, _(f[),WVyR(f[)6RQf[b5u~Sc4Y_c$OoxhKmv gPCQNwNՋHfN(f[),c[[=N, zQ(f[),؈ۏim, zMO(f[)nA CFD-based high-order Discontinuous Galerkin solver for three dimensional electromagnetic scattering problemsT[:_,_ O(f[),ؚ\qX(f[),Y[:_(f[)XMagnetism in oxygen-functionalized hexagonal boron nitride nanosheet on copper substrate퐇[ ,Ng퐇[ Journal of Physical Chemistry Cv 119,n 1,p 873-878[Numerical study on the power extraction performance of a flapping foil with a flexible tail4Tpg, f,u[,0ue[(f[)Physics of Fluids v 27,n 1,fAn adaptive immersed boundary-lattice Boltzmann method for simulating a flapping foil in ground effect4Tpg,N=N(f[), f,u[,sf(Y)COMPUTERS & FLUIDSwS: 106 u: 171-184aAeroacoustic investigation of a cavity with and without doors by delayed detached eddy simulation8International Journal of Aeronautical and Space Sciencesv 16,n 1,p 19-27UOn optimization of the observation station based on the effective independence methodDai, Guanbang(f[),~V[v 17,n 7,p 3735-3750122nd AIAA Computational Fluid Dynamics ConferenceStructural Health Monitoring and Integrity Management - Proceeding of the 2nd International Conference of Structural Health Monitoring and Integrity Management, ICSHMIM 20144Zheng, Zhaoyu(f[),h'Y_,Liu, Shulin(f[),Feng, Shuqing(f[)GProceedings of SPIE - The International Society for Optical Engineeringv 9524,VExperimental studies on finite element model updating for a heated beam-like structureY[QO(f[),u8l,wm\uIdentification of temperature-dependent thermal-structural properties via finite element model updating and selectionv 52-53,n 1,p 147-161?INTERNATIONAL JOURNAL OF APPLIED ELECTROMAGNETICS AND MECHANICS@Effect of torsional damping on aircraft nose landing-gear shimmyQޘ(f[),B[, _f,m_Nf(f[)v 52,n 2,p 561-568LMolecular dynamics study of a CNT-buckyball-enabled energy absorption systemKChen, Heng(f[),Zhang, Liuyang(f[),Becton, Matthew(f[),B[,Hё[,Wang, Xianqiao(f[)#PHYSICAL CHEMISTRY CHEMICAL PHYSICSwS: 17 g: 26 u: 17311-17321/International Journal of Control and Automation,The lightning protection of Mi-26 helicopterIET Seminar Digest v 2015,n 11,_A finite deformation constitutive model for thermally activated amorphous shape memory polymersv 26,n 12,p 1530-1538:The time-fractional diffusion equation for Woven composite N*(f[),hTPOAdvances in Civil Engineering and Building Materials IV - Selected and Peer Reviewed Papers from the 2014 4th International Conference on Civil Engineering and Building Materials, CEBM 2014 p 315-318KA micromechanical model on specific damping capacity caused by micro cracks sON(f[),hTPOv 17,n 4,p 1634-1644An experimental investigation of flow boiling heat transfer and pressure drop of R134a in a horizontal 2.168 mm tube under hypergravity. Part II: Heat transfer coefficient&s(f[),e$_,Li, Guohua(f[),Li, Dingkun(f[)/INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFERwS: 80 u: 597-604dIntelligent vibration control for high-speed spinning beam based on fuzzy self-tuning PID controller hTpQO(f[),HVs^SAnalysis of stiffness characteristics of a new fluid bag for axial shock protection _f,Jiang, Rui(f[),B[v 17,n 2,p 587-601aTrajectory tracking and vibration suppression of a 3-PRR parallel manipulator with flexible links  _l(f[),ё[ci,umuMULTIBODY SYSTEM DYNAMICSwS: 33 g: 1 u: 27-60|Effect of initial stress on propagation behaviors of shear horizontal waves in piezoelectric/piezomagnetic layered cylindersuf(f[),_NS, _Ux(Y),RёU(Y) v 63,p 47-53iEnhanced dielectric tunability of Ba x Sr 1x TiO 3  MgO composite ceramics co-modified with CuO and MnO 2$ T:_(f[),Du, Jianzhou ,(f[),؈ۏim,c[[=N,1gT[Qv 26,n 4,p 2107-2112UFabrication of macro piezoceramic fiber composite actuators by cutting-filling methodv 43,n 1,p 72-76"s[܏(f[),؈ۏim,c[[=N, _,Zhao, Jinling(f[)Structural Health Monitoring 2015: System Reliability for Verification and Implementation - Proceedings of the 10th International Workshop on Structural Health Monitoring, IWSHM 2015 v 1,p 617-624OInverse shape reconstruction of inner cavities using guided SH-waves in a platesl_,_NS,Hirose Sohichi(Y)cSemi-active vibration control based on unsymmetrical synchronized switching damping: Circuit designc[[=N,؈ۏim, _&(f[),B[v 27,n 8,p 1106-1120)Shadow removal based on YCbCr color space1g(f[),HNe,Yfh^(f[), _ؘs(f[)v 151,n P1,p 252-258RNumerical analysis of the plane waves scattering by semi-spherical Alluvial valley H\g,1gf[_l(f[)H\gyCOMPDYN 2015 - 5th ECCOMAS Thematic Conference on Computational Methods in Structural Dynamics and Earthquake Engineering p 4596-46037O(f[),YkSf,Wang, Liwei(f[),Wang, < Guoliang(f[),Xie, Fang(f[)v 9671,cMetamodel-based optimization of the bolted connection of a wing spar considering fatigue resistanceY)Y(f[),YkSf,R(f[),T(f[)v 230,n 5,p 805-814^Dynamic stall control on rotor airfoil via combination of synthetic jet and droop leading-edge,Annual Forum Proceedings - AHS Internationalv 1,n January,p 401-411BHighly-efficient aerodynamic design of rotor with high performance4T*t(f[),b/TQ,sZS,pSzf-f(f[)v 2,n January,p 817-827vNew trimming strategy for predicting of the unsteady aerodynamic characteristics of tilt-rotor/wing in conversion modev 1,n January,p 228-243hNumerical optimization for rotor blade-tip planform with low HSI noise characteristics in forward flightv 1,n January,p 67-75Mechanisms and Machine ScienceĞkSn,H^(f[), _^v 23,p 1133-1141ĞkSn,Y[h(f[), _^,N^Q,s[(Y)v 23,p 1121-1131OAnalytical investigation of dynamics of inflatable parabolic membrane reflector Ry[(f[),ё hs^!Journal of Spacecraft and Rocketsv 52,n 1,p 285-294ZConceptual design and experimental demonstration of a distributedly actuated morphing wing _s^(f[),hT=N, zepg(f[),m(Y)v 52,n 2,p 452-461;!^,Na,Qing, Xinlin P.(f[),Chang, Fu-Kuo(Y),Shi, Lihua(f[), v 221,p 41-52NCQ:_(f[),Na,,h[ޘ(f[) v 1,p 11-18SA spatial filter and two linear PZT arrays based composite structure imaging method,Rl_(f[),Na,\(f[)v 17,n 3,p 1218-1231 ,Na,Rl_(f[) v 2,p 570-576iOmni-directional damage detection and localization with a cruciform piezoelectric ultrasonic phased arrays_Q(f[),Na,,Rl_(f[)v 17,n 5,p 2338-2349hProviding multiradio wireless sensor network with high-throughput and long-distance transmitting abilityؚ\(f[),Na,,Q__(f[)p 19-24\Research on a strain-based shape reconstruction method using the fiber Bragg grating sensors땎sO(f[),Na,, _]].(f[) p 193-198 TvQ[(f[),Y_܏v 79,n 4,p 2325-2332ADamage detection of a bridge model based on strain modal analysissd_,Catbas, F.N.(Y),Celik, O.(Y)Life-Cycle of Structural Systems: Design, Assessment, Maintenance and Management - Proceedings of the 4th International Symposium on Life-Cycle Civil Engineering, IALCCE 2014 p 411-415>An infrasonic vibration energy harvester using pendulum impact ]\e(f[),Ov 47,n 2,p 467-474Physics ProcediaXSubset simulation for assessing structural reliability of multiple limit state functionswUNCECOMP 2015 - 1st ECCOMAS Thematic Conference on Uncertainty Quantification in Computational Sciences and Engineering p 209-217mNumerical analysis on thermo-mechanical behavior of shape memory alloy strip with two-way shape memory effectNg~Q,؈ۏim,c[[=N,Nie,Rui(f[)aASME 2015 Conference on Smart Materials, Adaptive Structures and Intelligent Systems, SMASIS 2015v 1,GCumulative second harmonics in a nonlinear transversely isotropic plateEuёs(f[),Chillara,VamshiK.(f[),Cho,Hwanjeong(f[),؈ۏim,Lissenden,CliffJ.(f[)lElectro-elastic fields around an elliptical hole in an electrostrictive plate: Isotropic and uncoupled cases _[Sun, Zhi (1); Sun, Jianhong (1); Zhao, Ming (1); Chen, Yue (1)RFlow field of cylindrical membrane inflation under the fluid-structure interactionGWang, Cong-Lei (1); Sun, Jian-Hong (1); Xu, Chang-Yue (1); Hou, Bin (1)37]Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astro41SDynamic loads and wake prediction for large wind turbines based on free wake methodVCao, Jiufa (1, 2); Wang, Tongguang (1); Long, Hui (2); Ke, Shitang (1); Xu, Bofeng (1)?Numerical analysis of sheet metal drawing and redrawing process&Dou, Shasha (1, 2); Xia, Jiansheng (2)eFeature recognition of ground target and position and attitude estimation for unmanned aerial vehicleCZhang, Liang (1); Xu, Jinfa (1); Xia, Qingyuan (2); Yu, Yongjun (1)An improvement and verification of position/attitude estimation algorithm based on binocular vision for unmanned aerial vehicleFZhang, Liang (1); Xu, Jin-Fa (1); Xia, Qing-Yuan (2); Yu, Yong-Jun (1)3SAR image matching algorithm based on improved-KAZEBYu, Yong-Jun (1); Xu, Jin-Fa (1); Zhang, Liang (1); Xiong, Zhi (2)LLADRC-based attitude decoupling control for helicopter and parameters tuningSWu, Chao (1); Wang, Haowen (2); Jiang, Chen (2); Zhang, Yuwen (2); Ni, Xianping (1)CSINS/GPS tightly integrated algorithm with gaussian particle filter@Yu, Yongjun (1); Xu, Jinfa (1); Xiong, Zhi (2); Zhang, Liang (1)\Fault diagnosis of non-stationary engineering system using cointegration coefficients matrix5Shi, Hai-Chen (1); Chen, Qian (1); Lin, Yuan-Ling (1)8A new type of large-thrust linear piezoelectric actuator5Zhu, Pengju (1); Shi, Yunlai (1); Zhao, Chunsheng (1)YDebonding characteristics and FBG monitoring analysis of CFRP T-joints under tensile load`Optimization of a multi-degree of freedom ultrasonic motor and its application on a x-y platform=Zhu, Hua (1); Wu, Wencai (1); Liu, Weidong (1); Pan, Song (1)nA Fractional Calculus Approach to the Prediction of Free Recovery Behaviors of Amorphous Shape Memory Polymers.Fang, C.-Q. (1); Sun, H.-Y. (1); Gu, J.-P. (2)YFinite element modeling and active vibration control of high-speed spinning flexible beam5Zhou, Lanwei (1); Chen, Guoping (1); Yang, Jingyu (2)ev 7lWater in Inhomogeneous Nanoconfinement: Coexistence of Multilayered Liquid and Transition to Ice Nanoribbons 7PStudy on the deterioration mechanism of concrete pavement for the deicer-scaling 7Extreme Wind Pressures and Non-Gaussian Characteristics for Super-Large Hyperbolic Cooling Towers Considering Aeroelastic Effect 7eStability and Reinforcement Analysis of Superlarge Exhaust Cooling Towers Based on a Wind Tunnel Test 7KDiscrete Optimum Design for Truss Structures by Subset Simulation Algorithm 7^Influence of Strake Wing on Unsteady Characteristics of an Aircraft Undergoing Lateral Motions 7 g Re,Article  7[Damage localization using warped frequency transform in active structural health monitoring 7Erratum: Stochastic resonance and stability for a time-delayed cancer growth system subjected to multiplicative and additive noises (Physica Scripta (2015) 90 (085201)) 7e YTPgehhS9_'`jRQ/cxvz 7SThree-Dimensional Reconstructed Finite Element Model for C/C Composites by Micro-CT 7 mRS-iWg'`OS 7 1b 7qKQ 7hbibce NܔQlvf_ˆ~oSvpe?@ABCDEFGHIJKLMNOPQRSTUVWXYZ[\]^_`abcefghijklmnopqrstuvwxyz{|}~W 1000 7WInitial stress correction method for the modeling of folded space inflatable structures 7HMPC based static aeroelastic numerical method for high aspect ratio wing 7H 7H 600 7EUniversity student cyber psychological fuzzy comprehensive evaluation 7HStudy of active network DC-DC boost converter based on switched-inductor 7JA continuum damage mechanics model for creep-fatigue life analysis of PMMA 7hStacking sequence design of composite thin-walled structure based on low energy impact damage resistance 7Z 7eReduction of stray corrosion by using iron coating in NaNO3 solution during electrochemical machining 7SRobust controller design of a class of uncertain switched fuzzy systems with delays 7b1443. 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Yu, Li (1); Yang, Xue (1); Cheng, Han (1) 7YO 7Aviation 718 7AHuang, Wei (1); Lu, Zhiliang (1); Tang, Di (1); Guo, Tongqing (1) 7]Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astro 740 710 7KNanjing University of Aeronautics and Astronautics, Nanjing, Jiangsu, China 7Liu, Yong (1); Li, Shanshan (2) 7 BioTechnology: An Indian Journal 729 7DDiangong Jishu Xuebao/Transactions of China Electrotechnical Society 7Jiangsu Key Laboratory of New Energy Generation and Power Conversion, Nanjing University of Aeronautics & Astronautics, Nanjing, China 7Wang, Ting (1); Tang, Yu (1) 7BNanjing University of Aeronautics and Astronautics, Nanjing, China 7=Yang, Chen (1); Wang, Ye (1); Mao, Ling (1); Xie, Shaojun (1) 76Dianji yu Kongzhi Xuebao/Electric Machines and Control 7;Zhu, Hua (1); Wu, Wen-Cai (1); Pan, Song (1); Jian, Lei (1) 736 7KEnergy Education Science and Technology Part A: Energy Science and Research 732 73Huang, Aifeng (1); Yao, Weixing (2); Chen, Fang (2) 7YkSf 735 7%Zhang, Pengfei (1, 2); 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Ji, Ruinan (1); Cao, Bingxin (1) 7 Chen, Zhe (1); Chen, Guoping (1) 72Zhendong yu Chongji/Journal of Vibration and Shock 733 7PPu, Yu-Xue (1); Zhang, Fang (1); Jiang, Jin-Hui (1); Xu, Jing (1); Jiang, Qi (1) 7 _e 7;Sun, Dong-Yang (1); Chen, Guo-Ping (1); Wang, Tie-Cheng (1) 7EWang, Ming-Yi (1); Ji, Hong-Li (1); Qiu, Jin-Hao (1); Zhang, Chao (1) 7ANew type of multi-point updating strategy for EGO parallelization%Xu, Shengguan (1); Chen, Hongquan (1)WSubsonic cavity noise prediction using stochastic noise generation and radiation method1Chen, Rongqian (1); Wu, Yizhao (1); Xia, Jian (1)TParallel numerical simulations of helicopter rotor flowfield based on zonal strategyALi, Peng (1); Zhao, Qijun (1); Zhao, Guoqing (1); Wang, Junyi (1)IResearch on impact characteristics of vertical water entry of a structure1Wu, Yungui (1); Chen, Huaihai (1); He, Xudong (1).Test method research on thermal modal analysis0Cui, Song (1); He, Xudong (1); Chen, Huaihai (1)H 600 7YInvestigation on near-wake vortices of wind turbine by numerical and experimental methodsWZhang, Zhenyu (1, 2); Xu, Bofeng (1); Wang, Long (1); Chen, Li (2); Wang, Tongguang (1)XNumerical simulations for active flow control of helicopter rotor based on synthetic jet"Zhao, Guoqing (1); Zhao, Qijun (1)2Research for dynamometer based on ultrasonic motor4Wen, Zhihui (1); Li, Huafeng (1); Zhang, Shaohua (2)WResearch on valveless piezoelectric pump with parallel connection conical spiral cavityACai, Jun (1); Huang, Jun (1); Hu, Fangjun (1); Zhang, Jianhui (1)7Structure design of the stepping Piezoelectric actuator-Liu, Weidong (1); Zhu, Hua (1); Cao, Ruyi (1)5A review of macro fiber composite and its applicationDi, Sisi (1); Li, Huafeng (1)pInvestigation on structural dynamic design and suspending characteristics of ultrasonic levitation type of gyros3Chen, Chao (1); Wang, Junshan (1); Liu, Tong (1, 2)AGeneric stiffness model for 3D woven orthogonal hybrid composites6Mahmood, Ansar (1); Wang, Xinwei (1); Zhou, Chuwei (1)NDynamic modeling and active vibration control of flexible parallel manipulatorXZhang, Quan (1); 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one-equation turbulence modelEBEffect of dual co-rotation wheels configuration on aircraft shimmyOLMolecular dynamics study of a CNT-buckyball-enabled energy absorption systemQNDynamics simulation study on civil aircraft planned pavement emergency landing`]Open/Closed-Loop Aeroservoelastic Predictions via Nonlinear, Reduced-Order Aerodynamic Models^[Equivalent Membrane Model for the Dynamic Analysis of a Prestressed Paraboloidal Cable NetsStability and mean extinction time for a metapopulation system subjected to two kinds of time delays and associated multiplicative and additive noiseswtElastic response of DNA molecules under the action of interfacial traction and stretching: An elastic thin rod model>;A flutter boundary prediction method for the three-dof wingnkAn insight into defect relaxation in metastable ZnO reflected by a unique luminescence and Raman evolutionsliHydroxylation of a metal-supported hexagonal boron nitride monolayer by oxygen induced water dissociationPMChemical 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Part II: Heat transfer coefficient96Vibration de-icing method with piezoelectric actuatorsGDModeling and calculation of open carbon dioxide refrigeration systemURResearch on safety analysis for airborne system based on extended functional modelifA Hybrid Method for Dynamic Mesh Generation Based on Radial Basis Functions and Delaunay Graph Mapping{xA three-dimensional explicit sphere function-based gas-kinetic flux solver for simulation of inviscid compressible flowsMJDelaunay graph and radial basis function for fast quality mesh deformationifAn adaptive immersed boundary-lattice Boltzmann method for simulating a flapping foil in ground effectb_Investigation of Low Heat Accumulation Asphalt Mixture and Its Impact on Urban Heat Environmentc`Thermal vibration of a single-walled carbon nanotube predicted by semiquantum molecular dynamicsjgAnalysis of frequency-dependent field-to-transmission line coupling with Associated Hermite FDTD methodLILateral compression behaviors of thin-walled equilateral triangular tubesHEInterface and Thermal Conductivity of Oxidized SiCp/5052Al CompositesEffect of Time Delay and Cross-Correlated Noises on Stochastic Resonance for a Metapopulation System with a Multiplicative Periodic Signal#e YTPgehhS9_'`jRQ/cxvzKHCritical plane approach to multiaxial variable amplitude fatigue loadingOCo-firing of PZT PMS PZN/Ag Multilayer Actuator Prepared by Tape-Casting Method^Temperature-Dependent Properties of a 1 3 Connectivity Piezoelectric Ceramic Polymer CompositeTQEpitaxial Growth and Multiferroic Properties of (001)-Oriented BiFeO3-YMnO3 FilmsjCrystal Structures and Properties of Pb(Ni1/3,Nb2/3) O3 Pb(Zr1/2,Ti1/2)O3 Thin Films on Silicon SubstratesurProperties of 0.96(Bi0.5Na0.5)TiO3-(0.04-x)BaTiO3-xLiNbO3 Lead-Free Piezoceramics Near Morphotropic Phase Boundary_A coupled immersed boundary lattice Boltzmann method and its simulation for biomimetic problems!”-hQlxx YTPgev Oa'`ZWVibration Reduction of a Bearingless Helicopter Rotor with 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Re @@@Sa@1b/bS)P(f[),ĞkSn,s[(Y),Y[h(f[) ĞkSnIQf[|[] z2015t^01g g Re @@@Tf@1b=Ğ(f[),sN(f[),b g(f[),z*mi(f[),ё[ci ё[ciMJZhendong Ceshi Yu Zhenduan/Journal of Vibration, Measurement and Diagnosisv 35,n 1,p 170-177 g Re @@@U`j@1bM%[ng(f[),NgNS\,Yang, Xixin(f[),Di, Sisi(f[) NgNS\MJZhendong Ceshi Yu Zhenduan/Journal of Vibration, Measurement and Diagnosisv 35,n 1,p 12-16 g Re @@@Vs@1bM%[rP[pg(f[),Y[_\,4Tёm(Y), _Q(f[), _olb(Y),h'Y_(Y) Y[_\MJZhendong Ceshi Yu Zhenduan/Journal of Vibration, Measurement and Diagnosisv 35,n 6,p 1012-1018 g Re @@@W{@1b/{g(f[),Y_܏,hg!j\(f[),R/c(f[) Y_܏=:Guangxue Jingmi Gongcheng/Optics and Precision Engineeringv 23,n 5,p 1358-1364 g Re @@@X |@1b#s_(f[),Y_܏,?QQ(f[) Y_܏ Jiqiren/Robotv 37,n 5,p 573-580 g Re @@@Y@1b?Liu, Weidong(f[),1gNS,hTv:_,}vNx,umu1gNSEBTransactions of Nanjing University of Aeronautics and Astronauticsv 32,n 2,p 180-186 g Re @@@Z`l@1b5Rch,Q,h'Y_,Wang, Guina(f[) RchEBTransactions of Nanjing University of Aeronautics and Astronauticsv 32,n 3,p 261-267 g Re @@@[e@1b1_(f[),f_,ѐ\*o(f[),!sޘ(f[) f_EBTransactions of Nanjing University of Aeronautics and Astronauticsv 32,n 4,p 452-460 g Re @@@\l@1bg2Wang, Yin(f[),Sun, Mengxin(f[),Huang, Weiqing(f[),RkSNS RkSNSMJZhendong Ceshi Yu Zhenduan/Journal of Vibration, Measurement and Diagnosisv 35,n 2,p 388-393 g Re @@@]l@1b W(f[),RkSNS,Q׋a RkSNSgdBeijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronauticsv 41,n 1,p 141-146 g Re @@@^3@1b f(f[),H~hQ H~hQEBTransactions of Nanjing University of Aeronautics and Astronauticsv 32,n 4,p 399-407 g Re @@@_4@1b ؚ\qX(f[),H~hQ H~hQ5uP[yb'Yf[f[b2015t^04g g Re @@@`V@1bY[_\,~t~g ~t~g2/Taiyangneng Xuebao/Acta Energiae Solaris Sinicav 36,n 10,p 2474-2478 g Re @@@apu@1b TOQ(f[),s_l\ s_l\gdBeijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronauticsv 41,n 11,p 2103-2109 g Re @@@bu@1b H\ z(f[),s_l\ s_l\EBTransactions of Nanjing University of Aeronautics and Astronauticsv 32,n 4,p 408-414 g Re @@@cv@1bf]NS(f[),s TIQ,gNX s TIQ ] zRf[2015t^09g g Re @@@d@1b#_=r(f[),u[,s%ffk,sN~u[.+Baozha Yu Chongji/Explosion and Shock Wavesv 35,n 3,p 326-334 g Re @@@ e@h@1bgNX,s TIQ gNX52Zhendong yu Chongji/Journal of Vibration and Shockv 34,n 18,p 33-38 and 44 g Re @@@ fh@1b9gNX,s TIQ,f]NS(Y),ug(Y),[T(Y) gNX2/Taiyangneng Xuebao/Acta Energiae Solaris Sinicav 36,n 1,p 33-40 g Re @@@ gi@1b7gNX,s TIQ,0N(f[),ug(Y),[T(Y) gNX(%Gongcheng Lixue/Engineering Mechanicsv 32,n 8,p 36-41 g Re @@@ hy@1b)Ng*mf(f[),4T~t,sU,\[^(f[)4T~tEBTransactions of Nanjing University of Aeronautics and Astronauticsv 32,n 5,p 579-584 g Re @@@ i y@1b!4T~t,1gx(f[),of[*(f[)4T~t ] zRf[2015t^02g g Re @@@ j0y@1b'ؚ2Z(f[),4T~t,sU,HG(f[)4T~tEBTransactions of Nanjing University of Aeronautics and Astronauticsv 32,n 3,p 297-304 g Re @@@ k|@1b%Ng~N5(f[),YO~S, _)Rf(f[) YO~STQYingyong Jichu yu Gongcheng Kexue Xuebao/Journal of Basic Science and Engineeringv 23,n 3,p 622-628 g Re @@@ l@^@1b3O,Tang, Qiang(f[),se(f[) OMJZhendong Ceshi Yu Zhenduan/Journal of Vibration, Measurement and Diagnosisv 35,n 2,p 203-211 g Re @@@m@1b85Zhu, Pengju (1); Shi, Yunlai (1); Zhao, Chunsheng (1) eЏegMJZhendong Ceshi Yu Zhenduan/Journal of Vibration, Measurement and Diagnosis35 g Re @@@n@1b@=Zhu, Hua (1); Wu, Wencai (1); Liu, Weidong (1); Pan, Song (1)1gNSMJZhendong Ceshi Yu Zhenduan/Journal of Vibration, Measurement and Diagnosis35 g Re @@@oW@1b%"Gao, Yukun (1); Chen, Hongquan (1) H~hQ74Dianbo Kexue Xuebao/Chinese Journal of Radio Science30 g Re @@@pw@1bYVCao, Jiufa (1, 2); Wang, Tongguang (1); Long, Hui (2); Ke, Shitang (1); Xu, Bofeng (1) s TIQEBTransactions of Nanjing University of Aeronautics and Astronautics32 g Re @@@qİ@1bVSWu, Chao (1); Wang, Haowen (2); Jiang, Chen (2); Zhang, Yuwen (2); Ni, Xianping (1) *PHQs^`]Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astro41 g Re @@@rܱ@1b96Mahmood, Ansar (1); Wang, Xinwei (1); Zhou, Chuwei (1) skO# Aerospace Science and Technology31 @p@s@1b#NgO(f[),b/TQ,1gy4Z(f[) b/TQ/,Annual Forum Proceedings - AHS Internationalv 1,n January,p 228-243 g Re @p@t0@1b uV^(f[),b/TQ b/TQ/,Annual Forum Proceedings - AHS Internationalv 1,n January,p 401-411 g Re @p@uh@1b 1gck(f[),b/TQ b/TQ/,Annual Forum Proceedings - AHS Internationalv 1,n January,p 67-75 g Re @p@v@1b)4T*t(f[),b/TQ,sZS,pSzf-f(f[) b/TQ/,Annual Forum Proceedings - AHS Internationalv 2,n January,p 817-827 g Re @p@w{@1b1Y)Y(f[),YkSf,R(f[),T(f[) YkSfc`Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineeringv 230,n 5,p 805-814 g Re @p@xʰ@1b85Zhou, Lanwei (1); Chen, Guoping (1); Yang, Jingyu (2) HVs^Journal of Vibroengineering17 g Re @p@y0w@1b s[(f[),skO skO/,Journal of Sandwich Structures and Materialsv 18,n 3,p 294-320 g Re @p@z$@1bI#Wang, Guina ,(f[),fwc,Mu, Hao(f[),h'Y_fwcPhotonic Sensorsv 5,n 2,p 116-122 g Re @p@{q@1b_.Qureshi, Ehtesham Mustafa(f[),lf,Chang, Lulu(f[)lf2/International Journal of Control and Automationv 8,n 6,p 121-138 g Re @p@|0s@1bE! _(f[),[O,eN(f[),Yy (f[),Xi Cao(Y) [O!Heat Transfer - Asian Researchv 44,n 8,p 753-764 g Re @p@ }T@1bAJun, Li(f[),ؚWO,Hong-Wei, Liu(f[) ؚWO!Open Civil Engineering Journal 9120-124 g Re @p@~ɰ@State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing, China;1.Fang, C.-Q. 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(2)Journal of Mechanics32 g Re @p@@NKNanjing University of Aeronautics and Astronautics, Nanjin, Jiangsu, China;)&Dou, Shasha (1, 2); Xia, Jiansheng (2)$!Metallurgical and Mining Industry7 g Re @p@j@1b _f(f[),Ng^l,N Ng^l41Hangkong Dongli Xuebao/Journal of Aerospace Powerv 30,n 6,p 1374-1381 g Re @@@j@1b _f(f[),Ng^l,N Ng^l:7Hangkong Xuebao/Acta Aeronautica et Astronautica Sinicav 36,n 7,p 2133-2144 g Re @@@z@1b S(f[),_VNS,SRpg _VNS:7Hangkong Xuebao/Acta Aeronautica et Astronautica Sinicav 36,n 9,p 2874-2883 g Re @@@z@1bE!Li, Ruirui(f[),^_im,hgkSN,Wu, Shen(f[) hgkSN:7Hangkong Xuebao/Acta Aeronautica et Astronautica Sinicav 36,n 6,p 1905-1914 g Re @@@X@1b#uV^(f[),b/TQ,4T*t(f[) b/TQ41Hangkong Dongli Xuebao/Journal of Aerospace Powerv 30,n 3,p 546-554 g Re @@@@1b/sO8(f[),b/TQ,l>x(f[),NgO(f[) b/TQ41Hangkong Dongli Xuebao/Journal of Aerospace Powerv 30,n 5,p 1267-1274 g Re @@@p@1b 1gck(f[),b/TQ b/TQ:7Hangkong Xuebao/Acta Aeronautica et Astronautica Sinicav 36,n 5,p 1442-1452 g Re @@@@@1bE!uV^(f[),b/TQ,~t~g,H ^(f[), _Q(f[),]O(f[) b/TQDALixue Xuebao/Chinese Journal of Theoretical and Applied Mechanicsv 47,n 2,p 351-355 g Re @@@@1b5lCQ(f[),fwm~g,Liu, Weidong(f[) fwm~g63Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinicav 32,n 3,p 815-822 g Re @@@@@1bK$NghsO(f[),HnfO,T[e(Y),m_m(Y),YckpQ(Y),f[N(Y) HnfO63Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinicav 32,n 2,p 571-578 g Re @@@A@1b Ng_(f[),HnfO HnfODALixue Xuebao/Chinese Journal of Theoretical and Applied Mechanicsv 47,n 3,p 458-470 g Re @@@B@1b=Ng_(f[),Nޘ(f[),HnfO,S:_(f[),Y[f_O(Y) HnfO63Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinicav 32,n 1,p 176-181 g Re @@@o@1b5Peng, Yiming(f[),B[, _f,O\B[:7Hangkong Xuebao/Acta Aeronautica et Astronautica Sinicav 36,n 6,p 1876-1884 g Re @@@ t@1bG"Wang, Yiding ,(f[),퐮N(f[),zfl, _wc(f[) zfl:7Hangkong Xuebao/Acta Aeronautica et Astronautica Sinicav 36,n 1,p 213-222 g Re @@@w@1b/s[,Ouyang, Xing(f[),YOĖ^s[63Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinicav 32,n 5,p 1487-1495 g Re @@@p@1bXUWu, Chao (1); 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