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_&l_&lODesign and application of servo system and its newtype control strategy for UAV Y[=NNS; __O; dl_hCModel identification of aircraft vertical tail using neural networkĞ^bskO?On a new crush trigger for energy absorption of composite tubes(International Journal of Crashworthinessyl _:_BFar-field sound radiated by elliptical vortex in an inviscid fluid0uO; hTPO hTPO KMulti-scale coupled numerical analysis of textile composites and structures _Nn; YO~S; Y[O; _^NOFlight dynamics characteristics of autorotating rotor/wing combination aircraft^SOqKQRRjPreparation and dynamic displacement testing of ionic polymer metal composites with platinum as electrodesO s TIQ`Numerical analysis of transition effect on stall performance of wind turbine airfoils and bladessSfm; fwc; h'Y_; ^IQ; R[g; _Sf=NKFiber Bragg grating pressure sensor for load monitoring of asphalt pavement>Yi Qi Yi Biao Xue Bao/Chinese Journal of Scientific InstrumenthgR; ĞĞ9The effects of variables on unsteady aerodynamic modeling0Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica0Gongneng Cailiao/Journal of Functional Materials4TOHNo[Identification method for helicopter fully coupled flight dynamics model in hover conditionNim B[B[JEffects of off-center location on aircraft attitude during catapult launch_Jisuanji Fuzhu Sheji Yu Tuxingxue Xuebao/Journal of Computer-Aided Design and Computer Graphics Nim B[O\wAnalysis on the dynamic characteristics of carrier-based aircraft nose landing gear with sudden holdback load dischargeTNanjing Li Gong Daxue Xuebao/Journal of Nanjing University of Science and TechnologyRey^; HNepAnalysis of load voltage and output power for Rainbow shape piezoelectric monomorph energy transferring elements3Fuhe Cailiao Xuebao/Acta Materiae Compositae SinicaLiu, Chen ,s_l\ O;FQs_l\1Extending Van Leer scheme for flows at all speeds=Deng, Jing-Hui (1); Tan, Jian-Feng (1); Zhang, Cheng-Lin (1) `Analysis of rotor dynamic response during ramp increased collective pitch by time-step free wake hTz܀; fSf; }vNx$Wing stall control by flow deflector/Taiyangneng Xuebao/Acta Energiae Solaris Sinica _Sf=Nh'Y_bS TNfwc?A high reliable optic fiber Bragg grating sensor network designf]NSs TIQELQG/LTR robust control in variable-pitch variable-speed wind turbineshgOONa _pgchfNSADesign of bio-inspired self-healing wireless sensor network nodes\ umu HCharacteristics of the thermopiezoelectric stator of an ultrasonic motorNg_RYkSfXNominal stress approach for life prediction of notched specimens under vibration loading>OR; HNoAConceptual design method for helicopter with main and tail rotorsBResearch on fiber gas sensor system based on scanning light sourceOs TIQ7Numerical analysis of the wind turbine blade-tip vortex RR; H(t; _HTg>Dynamic stall model for high maneuvering flight of helicopters hT[[RkNgeck2An awareness model for airplane cooperative design sёOё2uciumuё2uciJVelocity stability research of traveling wave type rotary ultrasonic motorTMulti-objective optimization design of wind turbine blades based on improved NSGA-II _s^ё hs^ё hs^GControl of arresting process for carrier aircraft considering kink-wave vPu[R^fsN~RA ghost cell method on finite volume adaptive Cartesian grids and its applicationsNg܀[; RHQe[Moment Lyapunov exponent for a co-dimension two-bifurcation system excited by a white noiseDHarbin Gongye Daxue Xuebao/Journal of Harbin Institute of TechnologyRchh'Y_:Interfacial shear strength between optical fiber and resinY[:Nl; 퐮N; zfl; c{vypPost-buckling analysis and structure optimization of integral fuselage panel subjected to axial compression load [vts m_VNSRBVI noise radiation characteristics across advancing and retreating sides of rotor  sSf^; of; _Q~rThermal flutter analysis of panel and multi-objective optimization design considering variations of flow yaw angle _QRSf~QhTPOwOgU`Nonlinear analysis on mechanical performance of PC multi-girder structures under lateral loadingĞk _^{GY YPĞkSn umurDynamics analysis and experiment on the fishtailing type of valveless piezoelectric pump with rectangular vibrator  _^;{GY YPNAnalysis on flow field of piezoelectric pump with unsymmetrical slopes elementNFinite element simulation of low velocity impact damage on composite laminates0Analytical method for helicopter maneuver flightRStructural phase transition and failure of nanographite sheets under high pressure#Journal of Physics Condensed MatterYang, Meng (1); Huang, Da (1)RThe unsteady aerodynamic characteristics of coupled motion at high angle of attack  _]YkSfYO^*"Pre-corrosion fatigue notch factor8^&tNa7A design strategy of structual health management system~Q; Hs; _=N; RQModification and research on bending rigidity formula of reinforced concrete beamNgeHNoPFormulation and validation of a helicopter model for pull-up maneuver simulation S_O; R_:_; NeExperimental investigation on the aerodynamic characteristics of flexible wing MAV in horizontal gust<Shiyan Liuti Lixue/Journal of Experiments in Fluid Mechanics1gT[Q; ς3 lead-free piezoelectric ceramics and its properties2Wuji Cailiao Xuebao/Journal of Inorganic MaterialsMaterials LettershgV[HVs^OAdaptive iterative learning control for vibration of flexural rectangular plateChen, Q. ; Worden, K.oA Decomposition Method for the Analysis of Viscoelastic Structural Dynamics with Time-Dependent Poisson's Ratio sNH`wm:eNaActive H-infinity control of the vibration of an axially moving cantilever beam by magnetic force(MECHANICAL SYSTEMS AND SIGNAL PROCESSINGS:_HnfOHnfOPrediction of the Strength Parameter of Cohesive Zone Model for Simulating Composite Delamination by the Equivalent Inclusion MethodPOLYMER COMPOSITES uNЏNёwmlNЏN`A Layout Optimization Method of Composite Wing Structures Based on Carrying Efficiency CriterionMStress corrosion of concrete exposed to the action of freezing-thawing cycles`Tumu Jianzhu yu Huanjing Gongcheng/Journal of Civil, Architectural and Environmental Engineering _Nn; YO~S; Y[O; RO _^N[Effect of magnesium sulfate solution on frost resistance of concrete under stress conditionRJiaotong Yunshu Gongcheng Xuebao/Journal of Traffic and Transportation EngineeringR^ ؈ۏim 8^Opg c[[=N 1gT[QnMetal core piezoelectric ceramic fiber rosettes for acousto-ultrasonic source localization in plate structures sr _eHVs^OResponse mapping technique of structural dynamics based on finite element modelYy loQf`Experimental investigation of flow characteristic of air-water two-phase flow under high gravityETransactions of the Japan Society for Aeronautical and Space Sciences]OofIAeroelastic simulation of limit-cycle-oscillation of a cropped delta wingNaMultiple impact source imaging and localization on composite structure based on Shannon complex wavelet and time reversal focusing^S 7(Wang, Yunhai ; Wang, Fanglei ; An, YukunUExistence and multiplicity of positive solutions for a nonlocal differential equationYang, J. 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B.FDelay-improved signal propagation in globally coupled bistable systemsu8l0wm\JParameterized aeroelastic modeling and flutter analysis for a folding wing^ef0؈ۏim01gT[Q0\g^hT`(K, Na)NbO3-based lead-free piezoelectric ceramics manufactured by two-step sintering ~l; h'Y_< ; fwc; zQuantum-behaved particle swarm optimization algorithm for the reconstruction of fiber Bragg grating sensor strain profilesOptics Communications kSl[$\Jisuan Lixue Xuebao/Chinese Journal of Computational MechanicsH~NOĞkSnĞkSnDesign and experiment of a single-phase-drive type linearly moving ultrasoni c motor(USM) with an inclined slider and a tower-shaped stator H^s[ĞkSnXo~gaMechanism and design of a linear motor with piezoelectric stacks basing on non-resonant vibration4TYkSfKTwo-level collaborative optimum design method for composite stiffened panel4T_lwms TIQ\Optimization design of airfoils for variable-pitch wind turbines based on genetic algorithmsbeP; __O; 1g)P; _x__OJResearch on large-deformation trapezoidal skin structure of morphing wingsY[_V1g zNe1g%fsFResearch of grid reconstruction on wing surfaces for icing calculationSRpg jgb/TQ_VNSERotor blade-vortex interaction noise prediction based upon hybrid CFD%Yuhang Xuebao/Journal of Astronautics8Jixie Gongcheng Xuebao/Journal of Mechanical Engineering9Wind turbine performance analysis with aeroelastic effect YvR O;FQT[:_XParallel computation of a high-order discontinuous Galerkin method on unstructured grids 4T_lwms TIQueNS2Design targets for wind turbine blade optimizationINumerical analysis and wake boundary modeling of wind turbine flow fields4Guangdianzi Jiguang/Journal of Optoelectronics LaserPm; c\O; ѐO; gmeFAn algorithm of filtering background noise of optical fiber gas sensorsss TIQ hg^NS; hh; RHQe se\RsOhTIQfse\IFinite element analysis of damage behavior of 3D woven tubular compositessNSfs[fksNSf<Numerical method for computing modal damping of rotor system  _s; NЏN; RkSA surrogate model-based optimization method for a lifting-body configuration designT[kS~HNoT[kS~XEffect of reverse flow region on characteristics of compound high speed helicopter rotor hgR; Ğ; 4T9htQFIdentification of unsteady aerodynamic model based on wind tunnel testR=N=N; eim; ё hs^; wm\eim_Three-dimensional optimal control of orbit transfer for an electrodynamic tethered subsatelliteNg9NYkSfDTwo-level optimization for GFRP wind turbine blade structural designnInvestigation of aerodynamic characteristics Predicting method for the helicopter rotor at high advanced ratiofNNHNoRInvestigation on nacelle conversion envelope analysis method of tiltrotor aircraft_[N̑HNoSTrajectory optimization of helicopter autorotation landing after one engine failure ?belB[NimMCarriered-aircraft taking-off with nose landing gear on ski-jump ramp profilesёOeЏeges2 Sf2 umuSPerformance of ultrasonic motor servo control system under high and low temperature1g zssY[_VNe1g%fs;Numerical study of wind turbine blade airfoil ice accretion fwc; h'Y_; _Sf=N; Ns; f^lNStudy on multi-channel optical fiber sensor based on surface plasmon resonance^IQ hgge eSfR UO8le _wmNLCooling attribute and road performance of infrared radiation asphalt mixture  PNm; HNoVStability and control characteristic analysis for flight of helicopter with slung-load ĞR; Ng܀[; RHQegOn the moment Lyapunov exponent of a viscoelastic plate subjected to the excitation of wide band noisesALixue Xuebao/Chinese Journal of Theoretical and Applied MechanicsYO,gi]ё hs^WConfiguration computation for one-dimensional continuum during deployment and retrieval 0u3t3t u[ OvPDPlacement optimization of wind farm based on niche genetic algorithm Ts TIQl\YApplication of 3-D dynamic stall model in wind turbine aerodynamic performance prediction s[ё[ciĞkSnOModal testing method for rotary ultrasonic motor using in-plane travelling wave Os TIQs:_UNumerical simulation of transition effect on aerodynamic performance of aerofoil S809 _Rh; B[; Hё[; Ngz%fVInvestigation on the landing-impact tests of the lunar lander and the key technologiessO; Ng^lNg^l g{ B[ Hё[ N\_Design and deploying kinematic analysis of a new deployable and lockable soft-landing mechanism  O;FQ 0ufNs YeP6Unstructured grid methods for unsteady flow simulation T[:_; 1gVey; [_lR; O;FQT[:_HHigh-order discontinuous galerkin solution of linearized Euler equationsTN]; YkSfcEquivalent bending stiffness method for stacking sequence optimization of composite stiffened panel RNs; ^fk; H^aBuckling, post-buckling and collapse analysis of stiffened composite panels with debonding damage 'k3~O; Rf[:_Rf[:_gLongitudinal and lateral aerodynamic characteristics of aircraft with atop radome and their improvementH܏_f ؈ۏim c[[=N 1gT[QPTracking control of piezoelectric actuator system using inverse hysteresis model _wmO; fwch'Y_fwcNumerical simulation and experimental study of strain field for morphing wings based on distributed fiber bragg grating sensor networkNgO; qKQ; H[; _~; ς8lR< ; NzfkqKQ8Research of retractable grid applied to morphing winglethgŖmhT=N\Design and optimization of an ultrasonic stress wave sensor based on magnetostrictive effect S_O4T9htQ;ĞeThe validation of unsteady aerodynamic model based on the high amplitude harmonic rolling motion test NB[Hё[FImpact response analysis of payloads of lunar lander for lunar landingwmq; Y[O; _^N; qdWwFrost resistance of high-volume mineral admixture concrete exposed to attack of chloride, sulfate and their combination9\wm; YOĖ^QIntegration of manufacturing cost into structural optimization of composite wings Q׋a; NS; RkSNS; Q f; Rςf_UAnalysis of inerting process influenced by scrubbing efficiency in aircraft fuel tank,Yang, Jianhua ; Cai, Xiangmei ; Liu, XianbinRHQejThe maximal Lyapunov exponent for a three-dimensional system driven by white noise (vol 15, pg 3498, 2010)<COMMUNICATIONS IN NONLINEAR SCIENCE AND NUMERICAL SIMULATION&Zhao, Jiang ; Tian, Qiang ; Hu, Haiyanwm\QModal Analysis of a Rotating Thin Plate via Absolute Nodal Coordinate Formulation/JOURNAL OF COMPUTATIONAL AND NONLINEAR DYNAMICSYe, Qiang ; Chen, PuhuigPrediction of the cohesive strength for numerically simulating composite delamination via CZM-based FEM)Wang, Long ; Wang, Tong-guang ; Luo, Yuans TIQ _bbYkSfYkSfTAn improved multiaxial high-cycle fatigue criterion based on critical plane approach8FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURESl\s TIQ(Modeling three-dimensional dynamic stallؚX[l0Yiu-Wing MaiASingularities of an interface crack in electrostrictive materials.INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTUREShg^NS; hh;Ng܀[ RHQeOn stationary probability density and maximal Lyapunov exponent of a co-dimension two bifurcation system subjected to parametric excitation by real noise-INTERNATIONAL JOURNAL OF NON-LINEAR MECHANICS R^fu[vPu[jThe Ghost Cell Method and its Applications for Inviscid Compressible Flow on Adaptive Tree Cartesian Grids;Yang, Hui ; Chen, Puhui ; Jiang, Yunpeng ; Tohgo, KeiichiroXIncremental damage theory of particulate-reinforced composites with a ductile interphaseCOMPOSITE STRUCTURES  _Sf=Nh'Y_fwcgGenetic algorithm-support vector regression for high reliability SHM system based on FBG sensor network Optics and Lasers in EngineeringDynamic strain measurement using two wavelength-matched fiber Bragg grating sensors interrogated by a cascaded long-period fiber grating\g^hT0؈ۏim01gT[Q0^ef0WOEffects of Fe2O3 doping on the microstructure and piezoelectric properties of 0.55Pb(Ni1/3Nb2/3)O 3-0.45Pb(Zr0.3Ti0.7)O3 ceramics; hh; hg^NSRHQeBDelay-induced vibrational multiresonance in FitzHugh-Nagumo system ~*mGl 1gT[Q; ^ef;Synthesis of (K, Na) (Nb, Ta)O3 lead-free piezoelectric ceramic powders by high temperature mixing method under hydrothermal conditions _^ Ğk _^{GY YPTheory and experiment on the soft texture and conning shaped single valve piezoelectric pump with different interior and exterior taper ltQ[fSffSf?Characteristics and control of blade tip vortex of wind turbinedNanjing Hangkong Hangtian Daxue Xuebao/Journal of Nanjing University of Aeronautics and AstronauticsHsOgas TIQHAeroelastic responses calculation of wind turbine blade in yaw condition]Wind turbine aerodynamic performance prediction based on free-wake/panel model coupled methoddBeijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and AstronauticsS:_; Y; ; HnfO; Nge; gNWS^Numerical and experimental analysis on seven-point bending test of integrated composite panels1Hangkong Dongli Xuebao/Journal of Aerospace Power2Zhendong yu Chongji/Journal of Vibration and ShockNRRjThe stochastic stability of a Van der Pol-Duffing oscillator under a non-Gaussian colored noise excitationSMA1_s[ YTPgeW{d'`q_TvՋxvzwb_Sg9_QX'`H\fv_RBlylRgS]N'Yf[_%fÔ0skOLambl(W YTPgeg-N Odv1 gPCQ!jb Nwm^Rf[f[O4ls^NuQ0H0umu 1UxX02oRYec03YecWNя:WX`nmv&Tsyr'`RgLAnalysis and Design of Stator of Traveling Wave Type Rotary Ultrasonic Motor199-200TStudy on Transient Properties of Levitated Object in Near-Field Acoustic Levitation %COMMUNICATIONS IN THEORETICAL PHYSICS-Nyb 1119-1124 Qs N^Q umu 1Ux 2oRؚ 3ckؚN^QZVlYNpWX5u:glP[iddPge'`xvzmnN[\Zo9e'`ZVlYNpWX5u:giddPge'`xvzHckt^ 9\j N^Q umu1ZSXT 2ZSXu 3oRؚ 4ckؚUHMW-PE YTPge(uNLlWelX5u:g./cRWS*Nޘ0N^Q0hgm0ĞkSn0umu NyeWv_LlWS5ufh0cXn0NZS0Wjς1-N~ 2Yec03ZSX04YecfhJA piezoelectric single-crystal ultrasonic microactuator for driving opticsGIEEE Transactions on Ultrasonics, Ferroelectrics, and Frequency Control8Ultrasonic, Ferroelectrics and Frequency Control Society bS\0O0umuOLAnalyses of the Temperature Field of Traveling Wave Rotary Ultrasonic MotorsIEEE O0Ng[0hTёZ 1Yec02UxX03UxXWControlled adsorption of droplets onto anti-nodes of an ultrasonically vibrating needleJournal of Applied PhysicsVirtf[O9gO0Nelson Tjiu1Yec02,gyuvDependence of electric energy output from a lead zirconate titanate ceramic piezoelectric element on impact conditionsMaterials Chemistry and Physics12 O01gNS0Ng[ 1Yec0oRYec03UxXISound induced lobed pattern in aqueous suspension film of micro particles!Sensors and actuators: A Physical Elservier2g ё[ci0s[0hg0 _^1oRؚ02ZSX03Yec04Yecё[ci6Fluid Pump Using a Bar-shaped Piezoelectric Transducer)CHINESE JOURNAL OF MECHANICAL ENGINEERINGpEDITORIAL OFFICE CHINESE JOURNAL MECHANICAL ENGINEERING, 22 BAIWANZHUANG DAJIE, BEIJING, 100037, PEOPLES R CHINA ё[ci0l/c 0[ 1oRؚ02UxX03UxX6hWgb_S5u/cP[v~WX5u:g ё[ci0s[0hg0umu1oRؚ02ZSX03ckؚ04ckؚ8A Fluid Pump Using a Bar-shaped Piezoelectric Transducer -NV:gh] zbeHr Xo~g0ĞkSn0s[0umu1-N~02Yec03ZSXu04YecXo~gWNS5u\ORhVvv~5u:gSvQؚHeqR Xo~g0NgNS\0ĞkSn 1-N~02Yec03Yec_WX5u:gqRSvQOSxvz5u:gNc6Rf[bT\nt]'Yf[Xo~g0ĞkSn1-N~02YecWN3z['`tvMOn:O g|~^c6ReЏeg0Ngs[0umu0 _^eЏeg>A new type butterfly-shaped transducer linear ultrasonic motor eЏeg0umu0 _^ GContact analysis and modeling of standing wave linear ultrasonic motor EJOURNAL OF WUHAN UNIVERSITY OF TECHNOLOGY-MATERIALS SCIENCE EDITIONeЏeg0umuHA new standing-wave-type linear ultrasonic motor based on in-plane modes ULTRASONICS eЏeg0Ngss0umu 1^02UxX03Yecn_v~WX5u:g[P[vR`TRg hT=Ns^0Y[_\0umu 1ZSX02Yec02YecY[_\(uNvh_Ƌ+Rvyr_ Sel-NVVaVb_f[b -NVVaVb_f[f[Oke0N0Y[_\v~Xl5uR:g|[[MO|~MOn|nxc6R_yr5u:g-NV5uP[CQNLNOSO_yr5u:gN~NRO[Sf~0Y[_\  hb_Lhb;Nd\OKbv:ghN5uP[ V[:gh]N@\ybYё[ci0N9N9N0hg0NgCS0g 1oRؚ02UxX03Yec04ZSX05UxXhgWA linear ultrasonic motor using (K0.5Na0.5)NbO 3 based lead-free piezoelectric ceramics"Sensors and Actuators, A: Physical7Elsevier, P.O. Box 211, Amsterdam, 1000 AE, Netherlands 2010 EIVYR$N9N9N0NgCS0Choi JY0Choi, JW0 hg Yoon, SJ1UxX02UxX03UxX04ZSX05Yec06Yec`Low-Temperature Sintered Pb(Zr,Ti)O-3-Pb(Mn,Sb)O-3-Pb(Zn,Nb)O-3 for Multilayer Ceramic ActuatorsJapanese Society of Physics _^0YP[0Ğk0Qޘ0ĞO0umu1ckؚ02oRؚ03UxX04oRؚ05ZSX06ckؚ _^kTheory and experiment of the valveless piezoelectric pump using tubes with combinated shape of  Y and cone$Science China Technological Sciences-NVyf[b{GY0 _^0Ğk0YP[0ĞkSn0umu1ZSX02ckؚ03UxX04oRؚ05ckؚ06ckؚ|Principle and Experimental Verification of Caudal-fin-type Piezo-stack Pump with Variable-cross-section Oscillating Vibrator {GY0 _^0ĞkN>\͜S5uSvfGrelv!jbNՋ{GY0 _^0Ğk0YP[0ĞkSn1ZSX02ckؚ03UxX04oRؚ05ckؚN>\͜_S*bbFdR/cP[eS5uSXlv~g-NVyf[b%fIQf[|[:ghNirtxvz@b0-NVNhVNhf[O _JNS0HwmR0 _^0q9ho1ZSXT03ckؚ S5u_AmϑqR5unvxvzV]S5u_AmϑqR5unvxvz _JNS0HwmR0 _^0 _t^Y0q9hoS5uqR5un_>e5uVvxvz \0 _^0umuumuLlWelX5u:g)n^:WRgel-NV5u:g] zf[b-NV5u:g] zf[O _z\0hTv:_0umu0ؚX[l1UxX02oRؚ03ckؚ04ckؚhTv:_X5u:g[P[v{S 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P@- P@~ PA @~ Q@k@ QA! 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Al@A@@A$@ @Y @~ A @~ @Pv@ AO AP A~ A@@ AQ A E AR AS AT Al@A7@A@ @\ @~ A$@~ @v@ A AB AN~ A<@ A A E A A A Al@A<@A@ @ @~ A @~ @v@ A AB AN~ A<@ A A E A A A Al@A<@A@ @ @~ A @~ @v@ A AB AN~ A<@ A A E A A A Al@AE@A@ @ @~ A @~ @w@ A  AB AN~ A<@ A A E A! A" A# Al@A<@A@ @ @~ A @~ @w@ A* A A E] A+ A Al@A@@A? @^ @~ A @~ @ w@ A A A E] A A Al@A=@A@ @^ @~ A @~ @0w@ A AB AN~ A<@ A A E A A A Al@AE@A@ @ @~ A @~ @y@ AU AV A~ AD@ AW A E AX AY AZ Al@AR@A@ @" @~ A$@~ @`l@ A6 A7 A G A8 AG Fh@F<@F@ F HH~ A@~ @0@ A_ A` A~ AB@ A_ A E Aa A A Al@AE@A@ @ @~ A @Dl~ @@ AI Ac A E_ AJ A Al@A=@A@ @` @~ A @~ @@ Ab Ac A E_ Ad Aa Ad@A?A@ @~ A$@~ @@ A Ac A Eb A Aw Al@AE@A@ @c @~ A @~ @ @ Ab Ac A~ AG@ Ad A E Ae Af Ag Al@AP@ A Ag @" @~ A$@~ @@ A[ A A A[ A E A\ A A]~ Al@ A^~ A@_@~ @`@ A` A A Ed Aa A Al@A9@A@ @7 @~ A @~ @a@ A A A Ed A A Al@A=@A@ @x @~ A @~ @ a@ A A A Ed A Aw Al@AE@A@ @7 @~ A @~ @z@ An A? A;~ AD@ Ao A El Ap A A Al@AA@A@ @ @~ A @~ @}@ Ah Ai Aj~ AB@ Ak A El Am AG A Al@A=@A@ @ @~ A @~ @7@ A A AN~ AA@ A A Et A A A Al@A@@A@ @~ A@~ @=@ A A AN~ A@@ A A Et A A A Al@A>@A@ @~ A@~ @>@ A A AN~ A@@ A A Et A A Av Al@A?@A@ @~ A@~ @?@ A A AN~ AC@ A A Et A A A Al@A>@A@ @~ A@~ @@@ A A AN~ A@@ A A Et A A Av Al@A?@A@ @~ A@~ @6@ A A AN~ AC@ A A Et A A Av Al@A?@A@ @ @~ A @~ @B@ A A A As A Et A A A Al@A>@ A] @~ A@~ @8@ A A AN~ AA@ A A Et A A Av Al@A>@A@ @ @~ A @~ @:@ A A AN~ A@@ A A Et Ae A A Al@A<@A@ @ @~ A @~ @;@ A A AN~ A@@ A A Et A A A Al@AG@A1@ @ @~ A @~ @<@ A A AN~ A@@ A A Et A A A Al@A@@A@ @f @~ A @~ @@@ Aq A A Et Ar Ag~ Al@~ A@ @h @~ A$@~ @A@ A A A Et A Aw Ah@AE@A@ @i @~ A @~ @A@ A A% A As A Et A A A Al@AA@ A{ @ @~ A @~ @B@ Aq Ar A As A Et Au A Av Al@A8@ Aw @ @~ A @~ @C@ A Ar A As A Et A A A Al@A>@ A @ @~ A @~ @D@ A As A Et A A~ Ah@A9@A&@ @j @~ A @~ @E@ A| A% A As A Et A} A~ A Al@A<@A@ @k @~ A @~ @E@ Au A% A As A Et Av Aw Al@A9@A @ @l @~ A$@~ @F@ A Ar A As A Et A A A Al@A>@ A{ @ @~ A @~ @F@ Ax Ay A As A Et Az A Av Al@A>@ A{ @ @~ A @~ @I@ As A A Et At Am Al@AG@ @l @~ A$@DlF~ @I@ A A A~ A?@ A A Et A A A Al@A1@A@ @l @~ A$@~ @J@ A A A~ A?@ A A Et A A A Al@A8@A@ @ @~ A @~ @K@ A A A~ A:@ A A Et A A A Al@A8@A@ @ @~ A @~ @K@ A A A~ A@@ A A Et A A A Al@A?@A@ @ @~ A @~ @L@ A A A~ A@@ A A Et A A A Al@A8@A@ @ @~ A @~ @^@ A A A~ A:@ A A En A A A Al@A@A@ @~ A@~ @]@ AT A A En AU A Ah@A?@A&@ @o @~ A @~ @]@ A A A~ A=@ A A En A Ap Al@A;@A@ @q @~ A$@~ @^@ A A A~ A=@ A A En A A A Al@A8@A@ @ @~ A @~ @@^@ A A A En A A Ah@A?@A(@ @o @~ A @~ @^@ A A A~ A>@ A A En A A A Al@A@@A@ @ @~ A @~ @@_@ A A A~ A?@ A A Et A A A Al@A@@A$@ @o @~ A @~ @_@ A A A~ A?@ A A Et A A A Al@A@@A@ @o @~ A @~ @_@ A A A~ AB@ A A Et A A A Al@A8@A@ @ @~ A @~ @`@ A AE A~ AB@ A A Et A A A Al@A@@A"@ @o @~ A @~ @@`@ AN AO A Et AP AQ Al@A@A@ @~ A$@~ @b@ A AG A Er A A Al@A<@A@ @i @~ A @~ @c@ AF AG A Er AH A Al@A@@A&@ @f @~ A @~ @s@ A A A~ AF@ A A Et A A A Al@A>@A@ @~ A@~ @g@ An AK A Es Ao A Ap@A1@A@ @t @~ A @~ @g@ A AK A Es A Au Al@AT@A@ @t @~ A$@~ @h@ AJ AK A Es AL AM Al@A0@A&@ @" @~ A$@~ @ h@ A AK A Es A A Al@AE@A@ @U @~ A @~ @@h@ AK AK A Es AL A Al@A8@A@ @U @~ A @~ @`h@ A AK A Es A A Al@A8@A? @U @~ A @~ @h@ A_ AK A Es A` Aa Al@AG@A? @t @~ A$@~ @z@ A  A A~ A=@ A  A Et A  A A Al@A<@A@ @~ A@~ @}@ A A A~ AI@ A A Et A A A Al@A>@A@ A @@~ A@~ @}@ A A A~ AI@ A A Et A A A Al@A>@A@ @~ A@~ @}@ A A A~ AI@ A A Et A A A Al@A>@A@ @~ A@~ @}@ A A A~ AI@ A A Et A A A Al@A>@A@ @~ A@~ @}@ A A A~ AI@ A A Et A A Av Al@A>@A? @~ A@Dhl~ @@s@ A A A~ AB@ A A Et A A A Al@A1@A@ @v @~ A$@~ @_@ A AE A~ AB@ A A En A A A Al@AJ@AK@ @"~ A@~ @s@ A A A En A A Ah@A=@A&@ @w @~ A @~ @t@ A A A~ AA@ A A Et A A A Al@A$@A@ @ @~ A$@~ @v@ A A A~ A@@ A A Et A A A Al@A8@A@ @~ A$@~ @v@ A A A~ A@@ A A Et A A A Al@AK@A @ @x @~ A$@~ @ v@ A A A~ A?@ A A Et A A A Al@AG@A"@ @" @~ A$@~ @0v@ A A A~ AA@ A A Et A  A  A Al@AO@A@ @" @~ A$@~ @@v@ A A A Ey A A Al@A<@A@ @7 @~ A @~ @9@ A A AN~ A@@ A A Et A A A Al@A6@A @ @~ A@~ @C@ A Ar A As A Et A Ak A Al@A8@A@ @~ A@~ @D@ A A% A As A Et A A Av Al@A8@A@ @~ A@~ @J@ A A A~ A:@ A A Et A A A Al@AE@A@ @~ A@~ @ `@ A A A~ AB@ A A Et A A A~ Fh@~ @~@ A A A Ez A A Al@A<@A@ @{ @~ A @~ @@ A A A A A Et A A| Al@A.@ @" @~ A$@~ @@ A A A E} A A3 Ap@At@A@ @~ A @~ @X@ A A A~ A:@ A A E A A A Al@A@@A? 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@ @~ A @~ @q@ A  A A E A   A  A  Al@A<@A@ @ @~ A @~ @r@ A A A~ A;@ A A E A  A  A  Al@A@@  A @ @~ A @~ @H@ A A A~ A=@ A A E A  A  A  Al@AE@A? @~ A@~ @W@ A A A A A E A  A  A  Al@AS@A&@ @"~ A@~ @Z@ A A A~ A9@ A A E A  A  Al@A@A? @"~ A@~ @u@ A A A E A  A# Al@AA@A? @W @~ A @~ @u@ A AB A~ AD@ A A E A  A  A Al@A@W@A @ @" @~ A$@~ @0u@ A A A E A  A Ah@A.@A@ @ @~ A @~ @@u@ A A A~ A?@ A A E A  A  A Al@A.@A @ @ @~ A @~ @Pu@ A A A~ A?@ A A E A  A  A Al@A<@A$@ @ @~ A @~ @`u@ A A A~ A9@ A A E A  A  A Al@A<@A@ @ @~ A @~ @pu@ A A A~ A;@ A A E A  A  A Al@AJ@A@ @" @~ A$@~ @u@ A A A~ A;@ A A E A  A  A Al@A<@A? @ @~ A @~ @u@ A A A~ AB@ A A E A  A  A Al@AE@A$@ @" @~ A$@~ @u@ A A A~ A7@ A A E A  A  A Al@AO@A(@ @" @~ A$@~ @u@ A A A~ A9@ A A E A  A  A Al@AN@A? @" @~ A$@~ @u@ A A A~ A9@ A A E A  A  A Al@AU@A@ @" @~ A$@~ @ u@ A AB A~ AD@ A A E A  A  A Al@A?A@ @"~ A@~ @@ A A A~ A9@ A A E A  A  A Al@A@A@ @~ A@~ @x@ A A A~ A:@ A A E A  A  A Al@A<@A@ @ @~ A @~ @x@ A A A~ A;@ A A E A  A  A Al@AE@A@ @ @~ A @~ @x@ A A A~ A?@ A A E A  A  A Al@A?@A? 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Z@ Z@~ ZA @~ [@f@ [A' [A [A [A [A [E [A( [ A%[ Al@A6@A&@ [@ [@~ [A @~ \@f@ \A \A \A \A \A \E \A  \ A \ A\ Al@AC@A @ \@ \@~ \A @~ ]@l@ ]A ]A ]A ]E ]A ] A] Ah@A?@A(@ ]@ ]@~ ]A @~ ^@@m@ ^A6 ^A1 ^A ^E ^A7 ^ AN^ Ah@A@@A@ ^@ ^@~ ^A @~ _@`m@ _AG _AH _A~ _A:@ _A1 _A _E _AI _ A _ AJ_ Al@A?@A@ _@ _@~ _A @D<l`abcdefghijklmnopqrstuvwxyz{|}~~ `@m@ `AK `AL `A~ `A:@ `A1 `A `E `AM ` AN ` AO` Al@AB@A@ `@" `@~ `A$@~ a@m@ aAl aA1 aA aE aAm a Apa Ap@AP@A? a@ a@~ aA @~ b@m@ bA5 bA6 bA~ bA=@ bA1 bA bE bA7 b A8 b A9b Al@A`@A@ b@ b@~ bA$@~ c@m@ cAP cAQ cA~ cA=@ cA1 cA cE cAR c AS c ATc Al@A6@A@ c@ c@~ cA$@~ d@n@ dA/ dA0 dA~ dA=@ dA1 dA dE dA2 d A3 d A4d Al@At@A.@ d@" d@~ dA$@~ e@ n@ eAU eAV eA~ eA=@ eA1 eA eE eAW e AX e AYe Al@A4@A? e@" e@~ eA$@~ f@`n@ fA\ fA] fA~ fA>@ fA1 fA fE fA^ f A_ f A`f Al@A5@A? f@~ fA$@~ g@n@ gAa gAb gA~ gA=@ gA1 gA gE gAc g Ad g A`g Al@A5@A@ g@ g@~ gA$@~ h@n@ hA hA1 hA hE hA h ANh Ah@A@@A@ h@ h@~ hA @~ i@n@ iAe iAQ iA~ iA>@ iA1 iA iE iAh i A i AFi Al@A>@A@ i@ i@~ iA @~ j@o@ jAi jAj jA~ jA<@ jA1 jA jE jAk j Al j Amj Al@Az@A? j@" j@~ jA$@~ k@ o@ kAn kA0 kA~ kA=@ kA1 kA kE kAo k Ap k Aqk Al@AW@A@ k@ k@~ kA$@~ l@`o@ lA lA1 lA lE lA l Aul Ap@AC@A@ l@ l@~ lA @~ m@o@ mAv mAw mA~ mA=@ mA1 mA mE mAx m Ay m Am Al@AG@A@ m@ m@~ mA$@~ n@o@ nAz nAs nA~ nA=@ nA1 nA nE nA{ n A| n A}n Al@AI@A&@ n@" n@~ nA$@~ o@o@ oA~ oAs oA~ oA=@ oA1 oA oE oA o A o Ao Al@A6@A(@ o@ o@~ oA$@~ p@`|@ pA pA pA~ pA>@ pA pA pE pA p A- p Ap Al@A=@A@ p@~ pA@~ q@p@ qA qA qA~ qAI@ qA1 qA qE qA q A q AZq Al@A:@A? q@ q@~ qA$@~ r@|@ rA rA rA~ rA9@ rA rA rE rA r A r A r@~ rA@~ s@ p@ sA sA0 sA~ sAA@ sA1 sA sE sA s A s A4s Al@A e@A? s@ s@~ sA$@~ t@0p@ tA tA tA~ tA;@ tA1 tA tE tA t A t AJt Al@A?@A@ t@ t@~ tA @~ u@|@ uA uA uA~ uAB@ uA uA uE uA u A u Au Al@A?@A@ u@~ uA@~ v@|@ vA vA vA~ vA;@ vA vA vE vA v A v Av Al@A?@A@ v@~ vA@~ w@`p@ wA wA wA~ wAB@ wA wA wE wA w A w Amw Al@Ay@A? w@" w@~ wA$@~ x@@ xA xA xA~ xA:@ xA xA xE xA x A x Ax Al@A9@A@ x@~ xA@~ y@@ yA yA yA~ yA7@ yA yA yE yA y A y Ay Al@A>@A(@ y@~ yA@~ z@ e@ zA! zA zA zA zA zE zA& z Az Al@A3@ z@~ zA@~ {@f@ {A {A {A {A {A {E {A { A~ { Al@ { A {@"~ {A@~ |@l@ |A: |A; |A~ |AA@ |A1 |A |E |A | A | A<| Al@A`t@A``@ |@"~ |A@~ }@l@ }A= }A }A~ }AC@ }A1 }A }E }A> } A? } A@} Al@AA@A@ }@"~ }A@~ ~@@o@ ~Ar ~As ~A~ ~A=@ ~A1 ~A ~E ~At ~ Au~ Al@AC@A@ ~@"~ ~A@~ @o@ A A A~ AI@ A1 A E A  A  A Al@A@A? @"~ A@DlF~ @w@ A A< A E A  A& Al@A<@A@ @ @~ A @~ @w@ A; A< A E A=  A Al@A@@A$@ @ @~ A @~ @0x@ A A A E A  A Ah@A>@A@ @T @~ A @~ @@x@ A AAA A A E A  A A Al@AE@A? 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A A A A E A"  A# Al@A@@A@ @~ A@~ @@f@ A A A A A E A  A  A Al@AC@A? @~ A@~ @@n@ AZ AH A~ A=@ A1 A E A[  A  A Al@A1@A? @~ A@~ @{@ A AB A~ A>@ A A E A  A  A Al@A>@A @ @ @~ A @~ @{@ A A A~ A>@ A A E A  A  A Al@A4@A@ @" @~ A$@~ @{@ A A A~ A>@ A A E A  A  A Al@A@@A? @ @~ A @~ @|@ A A A~ A@@ A A E A  A  A Al@A?@A@ @ @~ A @~ @|@ Ad A A E Ae  AN Ah@A@@A@ @ @~ A @~ @ |@ A A A~ A@@ A A E A  A  A Al@A@A@ @ @~ A @~ @0|@ A A A~ A>@ A A E A  A  A Al@A@@A@ @ @~ A @~ @@|@ A A A~ A>@ A A E A  A%  A Al@A6@A@ @ @~ A @~ @P|@ A AE A~ A>@ A A E A  A  A Al@AE@A@ @ @~ A @~ @p|@ A A A~ A=@ A A E A  A  A Al@A @A@ @" @~ A$@~ @|@ A A A~ A=@ A A E A  AX  A Al@A4@A$@ @" @~ A$@~ @|@ A A A~ A;@ A A E A  A  A Al@AD@A? @ @~ A @~ @|@ A A A~ AB@ A A E A  Ak  A Al@A8@A@ @ @~ A$@~ @|@ A A A~ AB@ A A E A  A  A Al@A<@A? @ @~ A @~ @|@ A3 A A E A4  A Al@A?@A@ @ @~ A @~ @@ A A A~ AD@ A A E A  A  A Al@AC@A(@ @~ A@~ @p@ A A A~ AA@ A1 A E A  A Fh@A3@A@ ~ @@ A A A A A E A  A Al@A>@A@ @ @~ A @~ @@ A A A*~ AF@ A A E A  A Al@AC@A"@ @" @~ A$@~ @@ Ap A A E Aq  Au Ap@AC@A@ @ @~ A$@~ @@ A A A~ A<@ A A E A  A  A Al@AB@  A @ @~ A$@~ @Ȁ@ A A A~ AD@ A A E A  A  A Al@A;@  A @" @~ A$@~ @Ѐ@ Am A A E An  Ao Ah@A9@A&@ @ @~ A @~ @S@ A A A~ A:@ A A E A  A Al@AB@A n@ @~ A@Dl~ @@S@ A A A~ A:@ A A E A  A Al@AB@Am@ @~ A@~ @R@ A A AV~ AE@ A A E A  A  A Al@A?@A@ @ @~ A @~ @3@ A A A~ A>@ A A E A  A  A Al@AL@  A @" @~ A$@~ @5@ A A A~ A:@ A A E A  A  A Al@AA@A@ @ @~ A @~ @S@ A A A E A  A Al@AB@A@ @~ A@~ @l@ A A A~ AA@ A A E A  A  A Al@A>@A? @~ A@~ @``@ A A A~ AG@ A A E A  A  A Al@A`@  A @ @~ A$@~ @`@ A A A~ AG@ A A E A  A  A Al@A[@  A @ @~ A$@~ @`@ A A A~ AG@ A A E A  A  A Al@Ad@  A @ @~ A$@~ @`@ A AB A~ A<@ A A E A  A  A Al@AM@A(@ @" @~ A$@~ @@a@ A A A E A  A Al@A8@A@ @ @~ A @~ @`a@ A A A E A  A Ah@A>@AB@ @ @~ A @~ @a@ A A A E A  A Al@A?@A.@ @ @~ A @~ @r@ A# A A~ A9@ A A E A$  A%  A&~  Al@~  A@ @~ A@~ @@c@ A A A~ AG@ A A E A  A  A Al@A?@A@ @ @~ A @~ @`c@ A A A~ AG@ A A E A  A  A Al@A8@A@ @ @~ A$@~ @c@ A A A~ AG@ A A E A  A  A Al@A8@A@ @ @~ A @~ @c@ A  A A E A!  A Al@A?@A@ @ @~ A @~ @c@ AB AC A E AD  A Al@A?@A>@ @ @~ A @~ @r@ A' A A~ A9@ A A E A(  A)  A*~  Al@~  A@ @~ A@~ @d@ A A A E A  A Al@A?@A8@ @ @~ A @~ @ l@ A A A~ AA@ A A E A  A  A Al@A3@A$@ @ @~ A @~ @@l@ A  A  A~ AA@ A A E A   A   A  Al@A.@A@ @ @~ A @~ @pp@ A A A~ AB@ A A E A  A Al@A?@A? @ @~ A @~ @p@ A A& A~ AB@ A A E A  AS Al@A6@A@ @ @~ A$@~ @p@ A A A~ AB@ A A E A  A Al@AI@A@ @ @~ A$@~ @p@ A A  A~ AB@ A A E A  A Al@A:@A@ @ @~ A$@~ @P~@ AE AF AV~ AD@ A8 A E AG  A  AH Al@A@@A@ @~ A@~ @`~@ AI AF AV~ AD@ A8 A E AJ  A  AH Al@A@@A@ @~ A@~ @p@ AP AQ A~ A:@ AR A E AS  AT  AU Al@A @A @ @~ A@~ @]@ A A A~ A@@ A A E A  A  A Ap@AM@A(@ @"~ A@~ @ z@ A2 A3 A~ A<@ A- A E A4  A|  A5 Fh@AH@ @"~ A@D@lF~ @2@ A A A~ A9@ A A E A  A  A Al@A6@A&@ @~ A@~ @4@ A A A~ A>@ A A E A  A  A Al@A6@A1@ @~ A@~ @z@ A+ A, A~ AG@ A- A E A.  A/  A0 Al@Ad@A@ A1 @ @~ A$@~ @r@ A A A~ A=@ A A E A   A!  A" Al@A0@A"@ @~ A@~ @~@ A< A= A~ AE@ A8 A E A>  A  A @~ A@~ @1@ A A A~ AA@ A A E A  A~  Al@  A~ @}@ A? A A~ AE@ A8 A E A@  A  A Al@A?@A@ @ @~ A @~ @}@ AA AB A~ AE@ A8 A E AC  A  AD Al@A3@A@ @ @~ A @~ @~@ AX A8 A E AY  A: Ah@AJ@A(@ @ @~ A @~ @ ~@ Ar A8 A E As  A Ah@AG@A8@ @ @~ A @~ @0~@ A6 A7 A~ AH@ A8 A E A9  A:  A; Al@AK@A&@ @ @~ A$@~ @@~@ AZ A8 A E A[  AN Ah@A@@A@ @ @~ A @~ @p@ A5 AL A E A6  A Al@A8@A@ @ @~ A @~ @@ AK A0 A~ A;@ AL A E AM  AN  AO Al@A?@A2@ @ @~ A @~ @@ A  AL A E A  A Al@A?@A@ @ @~ A @~ @h@ AV AW A~ A>@ AR A E AX  AN  AO Al@A?@A@@ @ @~ A @~ @g@ A} A~ A~ A;@ A A E A  A  A Al@AF@A@ @ @~ A @~ @`g@ A A A~ A:@ A A E A  A[  A\ Al@A:@A&@ @~ A@~ @g@ A A A~ A;@ A A E A  A  A~  Al@~  A@~ @W@ A A A~ A:@ A A E\ A  A  A Al@A&@A>@ @~ A@~ @T@ AY AZ A~ A@@ A[ A E\ A]  A^  A;~  Al@  A_ @ @~ A$@~ @T@ A` Aa A~ A@@ A[ A E\ Ab  A  A~  Al@  Ac @ @~ A @~ @U@ A AE A~ A;@ A A E\ A  A  A Al@AH@A@ @" @~ A$@~ @U@ A A A~ AM@ A A E\ A  A  A Al@A?@  A @" @~ A$@~ @U@ A A A~ AM@ A A E\ A  A  A Al@AB@A@ @" @~ A$@~ @V@ A A A~ AM@ A A E\ A  A  A Ap@A@n@ @ @~ A @~ @@V@ A A A~ AM@ A A E\ A  A  A Al@A n@A@ @ @~ A$@~ @V@ A A A~ AM@ A A E\ A  A  A Ap@AH@A@ @" @~ A @~ @V@ A AE A~ A<@ A A E\ A  A  A Al@AH@A@ A @" @~ A$@~ @b@ Ao Ap A~ A8@ Am A E\ Aq  Ar  As Al@A@@A@ @~ A@~ @@W@ AH A{ A E\ AI  A~ Ah@A9@A&@ @ @~ A @~ @W@ Ay Az A~ AC@ A{ A E\ A|  A  A Al@AE@A@ @ @~ A @DjlF~ @q@ A A A~ A<@ A A E\ A  Ar  A Al@A@@A@ @~ A@~ @r@ A A A~ AH@ A A E\ A  A  A~  Al@~  A(@ @~ A@~ @@b@ Ak Al A~ A:@ Am A E\ An  A  A Al@AE@A@ @ @~ A @~ @`b@ At Au A~ A:@ Am A E\ Av  Aw  Ax Al@AB@A"@ @ @~ A @~ @`d@ A A A~ AB@ A A E\ A  A  A Al@AE@A@ @ @~ A @~ @`x@ A A A~ A?@ A A E\ A  A  A Al@A<@A@ @~ A@~ @q@ A A A~ A:@ A A E\ A  A  A Al@AB@A @ @ @~ A @~ @q@ A AAA A A E A  A A Ad@AJ@Ae@ A @ @~ A @~ @pr@ A A A~ AH@ A A E\ A  Ak  A Al@A8@A@ @ @~ A$@~ @@U@ A A A~ AM@ A A E\ A  A  A Al@A?A? @"~ A@~ @ d@ A A A~ AB@ A A E\ A  A  A~  Al@  A @"~ A@~ @@d@ A A A~ AB@ A A E\ A  A  A~  Al@  A @"~ A@~ @q@ A A A~ A=@ A A E\ A  A  A~  Al@  A  A @"~ A@~ @Px@ A A A~ A:@ A A E\ A  A  A Al@AE@A@ @ @~ A @~ @q@ A A A~ A<@ A A E\ A  A[  A Al@A:@A&@ @~ A@~ @{@ Ad Ae A~ AE@ Af A E\ Ag  A  A Al@AE@A@ @ @~ A @~ @px@ A A A~ A?@ A A E\ A  AG  AH Ap@A>@A? @~ A@~ @r@ A A A~ AH@ A A E\ A  A  A Al@A*@A@ ~ @p{@ Ah Ai A~ A;@ Af A E\ Aj  A  A~  Al@~  A?~ @x@ A A A E A  Aw Al@AE@A? @ @~ A @~ @@ A A A E A  A Al@A@@A@ @ @~ A @~ @@ A A A E A  A Al@A<@A@ @ @~ A @~ @@ A A A E A  Aw Al@AE@A@ @ @~ A @~ @@ A A A E A  A Al@A=@A@ @ @~ A @~ @? 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A@  A Al@A<@A@ @~ A@~ @`v@ AM A A~ A:@ AC A E  AN  A$  A% Al@A@@A@ @~ A@~ @pv@ AO A A~ A9@ AC A E  AP  A$  A% Al@A@@A&@ @~ A@~ @v@ AA AB A~ AG@ AC A E  AD  AE  AF  Al@AC@A@ @~ A@~ @`j@ A A: A E A  A  Ah@A;@A@ @ @~ A @~ @j@ AU AV A~ AI@ A: A E  AW  A  A  Al@AE@A@ @ @~ A @~ @j@ A] A^ A~ AI@ A: A E  A_  A  A  Al@A<@A@ @ @~ A @~ @j@ AD A: A E AE  Aw  Ah@AE@A@ @ @~ A @~ @z@ Au Av A~ A:@ AY A E  Aw  A6  A Al@A>@A@ @~ A@~ @z@ Aq Ar As~ AI@ AY A E  At  A6  A Al@A>@A? @~ A@~ @z@ Ax A AN~ A?@ AY A E  Ay  Ag  Ah Al@A;@  A @~ A@~ @{@ Ad Ae AN~ A?@ AY A E  Af  Ag  Ah Al@A;@  A @~ A@~ @{@ An Ao AN~ A?@ AY A E  Ap  A6  A Al@A>@A@ @~ A@~ @v@ AG A A~ AG@ AC A E  AH  AI  AJ Al@A@@A@ @ @~ A @~ @v@ AQ A A~ A8@ AC A E  AR  A Al@Ao@A@ @"~ A@~ @v@ AK A A AC A E  AL  A  A Al@A<@A@ @ @~ A @~ @v@ AS A A~ A8@ AC A E  AT  A Al@APp@A@ @"~ A@~ @y@ A A A E A  Aw Al@AE@A? @ @~ A @~ @ {@ AX A AN~ AA@ AY A E  AZ  A[  A\ Al@AE@A@ @ @~ A @~ @0{@ A` Aa AN~ AA@ AY A E  Ab  Ac  A Al@A,@A@ @ @~ A @~ @@{@ A AY A E A  A Ah@A$@A@ @ @~ A @~ @P{@ A AY A E A  A Ah@A@@A@ @ @~ A @~ @`{@ A AY A E A  A Ah@AC@A&@ @ @~ A @~ @[@ A0 A A A1 A E  A2  A3~  Al@~  A(@~ @ @ Az A{ A~ AG@ A| A E  A}  A~  AF Al@A@@A@ @ @~ A @~ @z@ Ai Aj AV~ AA@ AY A E  Ak  Al  Am~  Al@~  A&@Dl !"#~ @@ A A A~ A7@ A| A E  A  A  A~  Al@~  A"@~ !@@ !A !A !A ! 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