• 대한의용생체공학회:의공학회지
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• 제14권4호
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• pp.307-314
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• 1993

Plasma protein adsorption is the first event in the blood-material interaction and influenc- es subsequent platelet adhesion towards thlㅈombus formation. Thiㅈomboembolic events are strongly influenced by surface characteristics of materials and fluid dynamics inside the blood pump. In vitro flow visualizaion and an amimal experiment with the moving actuator type TAH were Performed in order to investigate fluid dynamic effects on the protein adsorption. The diffel'encl level, j of shear rate inside the ventricle Lvere determined by consid- ering the direction of the major opening of four healt valves in the implanted TAH and the visualized flow patterns as well. Each ventricle of the explanted TAH was sectionalized into 12 segments according to the shear rate level. The adsorbed protein on each segment was quantified using the ELISA method after soaking in 2% (wye)SDS/PBS for two days. Adsorbed protein layer thicknesses Itvere measured by the Immunogotd method under TEM. The SEM observation show that right ventricle (RV) , immobilized with albumin, displayed different degrees of platelet adhesion on each segment, whereas the left ventricle (LV), grafted by PEO-sulronate, indicated nearly , iame platelet adhesion behavior, regardless of shear rates. The surface concentrations of adsorbed proteins in the low shear rate region are hlghel'than those in the high region, which was confirmed statistically. A modified adsorption model of plasma protein onto polyurethane surface was suggested by considering the effect of the fluid dynamic characteristics.

• 한국항공우주학회지
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• 제46권3호
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• pp.197-209
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• 2018

본 연구에서는 전진 비행하는 쿼드 틸트 로터(Quad Tilt Rotor, QTR)에 대한 수치적 연구를 수행하여, 각 구성 요소에 의한 간섭효과와 위상차 및 로터 회전 방향 등 로터 운용조건에 의한 영향을 분석하였다. 효율적인 로터 유동장 계산을 위해 오픈소스 CFD 코드인 OpenFOAM에 Actuator Surface Method(ASM) 기법을 결합한 해석자를 사용하였다. 전 후방 날개의 양력은 날개 끝단에 부착된 로터의 회전 방향에 따라 증감하며 특히 후방 날개에서는 전 후방 로터에 의한 간섭효과가 복합적으로 나타난다. 전 후방 로터의 위상차에 의한 날개의 공력 성능 변화는 상대적으로 미미함을 확인하였다. 로터에서는 날개로 인한 폐쇄효과 발생에 따라 국소적으로 높은 추력이 발생한다. 특히, 후방 로터에서는 전방 나셀에서 발생한 후류의 간섭효과로 인해 전방 로터 대비 높은 국소적 추력이 발생한다. 또한 로터 간의 위상차에 따라 추력 요동의 진폭이 감소할 수 있음을 확인하였으며 운용 조건에 따른 전 후방 로터의 성능과 전체 비행체의 공력 성능을 비교, 분석하였다.

• 한국항공우주학회지
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• 제40권2호
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• pp.165-170
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• 2012

본 논문에서는 비행체 날개의 조종면에 작용하는 힌지 모멘트 분석을 위한 시험적 방법 및 결과를 수록하였다. 비행 공력 하중에 의하여 조종면에 힌지 모멘트가 작용할 경우, 조종면 구동장치에서 측정된 각도와 실제 조종면의 각도 사이에 탄성 변형에 의한 차이가 발생하며, 이 차이를 측정하여 힌지 모멘트로 환산할 수 있다. 이를 위하여 지상에서 조종면 구동장치 시스템의 비틀림 강성을 측정하기 위한 정하중 시험 및 조종면 각도 센서 교정시험을 수행하였다. 이 결과를 이용하여 비행 중 작용하는 힌지 모멘트를 계산할 수 있으며, 또한 체결부위의 미끄러짐 및 백래시 등의 기계적 오차도 예측할 수 있다. 실제 비행시험 결과를 이용하여 조종면에 작용한 힌지 모멘트를 계산한 결과와 수치 해석 결과의 비교를 통하여, 제시된 하중 측정 방법의 타당성을 입증하였다.

• 로봇학회논문지
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• 제2권4호
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• pp.353-360
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• 2007

This paper proposes the trot gait pattern generation and online control methods for a quadruped robot to carry heavy loads and to move fast on uneven terrain. The trot pattern is generated from the frequency modulated pattern generation method based on the frequency modulated oscillator in order for the legged robots to be operated outdoor environment with the static and dynamic mobility. The efficiency and performance of the proposed method are verified through computer simulations and experiments using qRT-1/-2. In the experiments, qRT-2 which has two front legs driven by hydraulic linear actuators and two rear casters is used. The robot can trot at the speed up to 1.3 m/s on even surface, walk up and down the 20 degree inclines, and walk at 0.7 m/s on uneven surface. Also it can carry over 100 kg totally including 40 kg payload.

• Composites Research
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• 제24권6호
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• pp.12-17
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• 2011

자체-센서와 미세 작동기 응용을 위한 CNT와 ITO로 코팅된 나노복합재료의 계면접착 내구성과 전기적 특성을 평가하였다. 나노복합재료의 접착 및 계면 내구성은 반복하중 피로시험에 따른 전기저항도를 측정하여 평가하였다. CNT와 ITO의 고유 전기적 특성으로 인하여 CNT가 코팅된 PVDF 나노복합재료는 ITO가 코팅된 경우보다 다소 낮은 전기저항도를 나타내었으나, 모두 양호한 자체-감지능을 보여주었다. CNT/PVDF와 ITO/PVDF 나노복합재료 모두 계면 내구성은 양호함을 확인하였다. 정적 접촉각 시험을 통해 CNT와 ITO 그리고 PVDF간의 표면에너지, 접착일, 그리고 퍼짐계수를 평가하여 계면 내구성과 의 상호 관련성을 확인하였다. 수용액에서 CNT와 ITO로 코팅된 PVDF 시편의 최적의 작동성은 주파수와 전압을 달리하여 레이져 변위센서를 사용한 연신율 변화로 측정하였다. 작동된 두 나노복합재료들의 연신율은 주파수가 증가함에 따라 감소하며, 반면에 전압의 증가에 따라 상승하였다. 각 나노복합재료의 나노구조 및 고유의 전기적 특성으로 인하여, CNT/PVDF가 ITO/PVDF 보다 자체-감지 및 작동기로서 더 적합하다는 것을 알 수 있었다.

• Smart Structures and Systems
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• 제25권6호
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• pp.643-655
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• 2020

Active control of nonlinear vibration of stiffened functionally graded (SFG) cylindrical shell is studied in this paper. The system is subjected to axial and transverse periodic loads in the presence of thermal uncertainty. The material composition is considered to be continuously graded in the thickness direction, also these properties depend on temperature. The relations of strain-displacement are derived based on the classical shell theory and the von Kármán equations. For modeling the stiffeners on the cylindrical shell surface, the smeared stiffener technique is used. The Galerkin method is used to discretize the partial differential equations of motion. Some comparisons are made to validate the SFG model. For suppression of the nonlinear vibration, the linear and nonlinear control strategies are applied. For control objectives, the piezoelectric actuator is attached to the external surface of the shell and the thin ring piezoelectric sensor is attached to the middle internal surface of shell. The effect of PID, feedback linearization and sliding mode control on the suppression of vibration for SFG cylindrical shell is presented.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2006년도 제37회 하계학술대회 논문집 C
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• pp.1621-1622
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• 2006

This paper presents the effect of driving waveform for piezoelectric bend mode inkjet printhead with optimized mechanical design. Experimental and theoretical studies on the applied driving waveform versus jetting characteristic s were performed. The inkjet head has been designed to maximize the droplet velocity, minimize voltage response of the actuator and optimize the firing frequency to eject ink droplet. The head design was carried out by using mechanical simulation. The printhead has been fabricated with Si(100) and SOI wafers by MEMS process and silicon direct bonding method. To investigate how performance of the piezoelectric ceramic actuator influences on droplet diameter and droplet velocity, the method of stroboscopy was used. Also we observed the movement characteristics of PZT actuator with LDV(Laser Doppler Vibrometer) system, oscilloscope and dynamic signal analyzer. Missing nozzles caused by bubbles in chamber were monitored by their resonance frequency. Using the water based ink of viscosity of 4.8 cps and surface tension of 0.025N/m, it is possible to eject stable droplets up to 20kHz, 4.4m/s and above 8pL at the different applied driving waveforms.

• Steel and Composite Structures
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• 제37권2호
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• pp.229-251
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• 2020

In this paper, dynamic buckling of a smart sandwich nanotube is studied. The nanostructure is composed of a carbon-nanotube with inner and outer surfaces coated with ZnO piezoelectric layers, which play the role of sensor and actuator. Nanotube is under magnetic field and ZnO layers are under electric field. The nanostructure is located in a viscoelastic environment, which is assumed to obey Visco-Pasternak model. Non-local piezo-elasticity theory is used to consider the small-scale effect, and Kelvin model is used to describe the structural damping effects. Surface stresses are taken into account based on Gurtin-Murdoch theory. Hamilton principle in conjunction with zigzag shear-deformation theory is used to obtain the governing equations. The governing equations are then solved using the differential quadrature method, to determine dynamic stability region of the nanostructure. To validate the analysis, the results for simpler case studies are compared with others reported in the literature. Then, the effect of various parameters such as small-scale, surface stresses, Visco-Pasternak environment and electric and magnetic fields on the dynamic stability region is investigated. The results show that considering the surface stresses leads to an increase in the excitation frequency and the dynamic stability region happens at higher frequencies.

• Journal of Advanced Marine Engineering and Technology
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• 제27권5호
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• pp.590-599
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• 2003

In this study. object transport method based on ultrasonic flexural vibration is presented. Ultrasonic vibration generates ultrasonic traveling waves on the surface of elastic medium. Objects are transported through the interaction with traveling waves propagating in medium. Two types of transport methods are studied： frictional drive and acoustic levitation. With frictional drive, objects are transported in contact with the beam in the opposite direction of wave propagation whereas with acoustic levitation, objects are acoustically levitated above the beam surface and transported in the wave propagation direction. Transport characteristics are experimentally investigated using objects of different shapes and sizes. The transition from acoustic levitation mode to frictional drive mode is also examined. and it is found to occur when the ratio of mass to area of an object exceeds the threshold ratio of mass to area. It is envisaged that this feasibility study will serve as a stepping-stone for ultrasonic vibration to become an effective industrial material handling device in the future.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2013년도 춘계학술대회 논문집
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• pp.522-527
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• 2013

In this study, dynamic response control of a flexible wing such as gust loads alleviation using sliding mode control method is presented. To achieve this purpose, trailing edge control surface of a flexible wing is used as control means generating the aerodynamic control force. Aeroservoelastic CASE) model consisting of aeroelastic plant, control surface actuator model, and gust model depicting the atmospheric turbulence is formulated in the state space. A sliding mode controller based on the estimated state vector is designed for active dynamic response control of flexible wing aeroservoelastic model. The performance of the controller designed is demonstrated via numerical simulation for the representative flexible wing model under atmospheric turbulence loading.