• 한국측량학회지
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• 제20권1호
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• pp.77-83
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• 2002

최근 산업의 발달로 도시가 확장되고 건설현장이 대형화됨에 따라 지하 시설물에 대한 정보가 필수적이다. 이 논문에서는 730 MHz 의 고정 주파수를 방사하는 3소자 안테나 방식의 GPR을 이용하여 자체 제작한 시험장 속에 매설된 다양한 시험편의 검출능력을 조사하였다. 여러 가지 상황에 대한 검출능력을 알아보기 위하여 매설물의 재질, 크기, 매설 깊이에 차이를 두어 실험을 수행하였다. 레이다파의 전파속도를 조절하여, B-scan상의 쌍곡선 패턴의 위치를 실제 매설한 깊이에 정확하게 일치하도록 함으로써 실험결과로부터 얻은 지반에서의 레이다파의 전파속도가 기존 자료와 유사함을 확인하였다.

• Fibers and Polymers
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• 제5권2호
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• pp.122-127
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• 2004

In this study, we evaluated the effect of the molecular weight of the polymer on electrospun poly(ethylene terephthalate) (PET) nonwovens, and their mechanical properties as a function of the linear velocity of drum surface. Polymer solutions and electrospun PET nonwovens were characterized by means of viscometer, tensiometer, scanning electron microscope(SEM), wide angle X-ray diffraction measurement (WAXD) and universal testing machine (UTM). By keeping the uniform solution viscosity, regardless of molecular weight differences, electrospun PET nonwovens with similar average diameter could be obtained. In addition, the mechanical properties of the electrospun PET nonwovens were strongly dependent on the linear velocity of drum surface. From the results of the WAXD scan, it was found that the polymer took on a particular molecular orientation when the linear velocity of drum surface was increased. The peaks became more definite and apparent, evolving from an amorphous pattern at 0 m/min to peaks and signifying the presence of crystallinity at 45 m/min.

• Steel and Composite Structures
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• 제17권2호
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• pp.199-213
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• 2014

The damage characters of scarf repaired composite laminates subjected to low-velocity impact with various energy levels at different locations are studied experimentally. The results are compared with those of the original laminates which have no initial damage and don't need repair. The impact load-time history of the specimens, the velocity-time curves of the impactor, the post impact compressive strength of the specimens and the C-scan photographs of the damaged regions are obtained. The delamination threshold load and damage character of the specimen section at impact point are also studied. The results have shown that the impact response of a repaired composite laminate is sensitive to the location of the impact. The impact load and the delamination threshold load have shown different characters for specimens with different impact locations. The debonding characters of the adhesive and compressive strength after impact of the specimens are also influenced by impact locations.

• International Journal of Aeronautical and Space Sciences
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• 제16권2호
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• pp.190-205
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• 2015

In this paper, the impact damage behavior of USN-150B carbon/epoxy composite laminates subjected to high velocity impact was studied experimentally and numerically. Square composite laminates stacked with $[45/0/-45/90]_{ns}$ quasi-symmetric and $[0/90]_{ns}$ cross-ply stacking sequences and a conical shape projectile with steel core, copper skin and lead filler were considered. First high-velocity impact tests were conducted under various test conditions. Three tests were repeated under the same impact condition. Projectile velocity before and after penetration were measured by infrared ray sensors and magnetic sensors. High-speed camera shots and C-Scan images were also taken to measure the projectile velocities and to obtain the information on the damage shapes of the projectile and the laminate specimens. Next, the numerical simulation was performed using explicit finite element code LS-DYNA. Both the projectile and the composite laminate were modeled using three-dimensional solid elements. Residual velocity history of the impact projectile and the failure shape and extents of the laminates were predicted and systematically examined. The results of this study can provide the understanding on the penetration process of laminated composites during ballistic impact, as well as the damage amount and modes. These were thought to be utilized to predict the decrease of mechanical properties and also to help mitigate impact damage of composite structures.

• 대한전기학회논문지
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• 제35권11호
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• pp.519-528
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• 1986

By using a least-square input estimator and likelihood ratio technique, a tracking problem is presented. A Kalman tracking filter based on constant-velocity, straight-line model is used to track a target and the filtered estimate is updated using an input estimate when a maneuver is detected. Track residuals at each scan are sensed by a detector to guard against unexpected corrections of the filter. The simulation results show there are significant improvements using the scheme presented.

• 비파괴검사학회지
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• 제29권6호
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• pp.586-590
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• 2009

Poisson's ratio, one of elastic constants of elastic solids, has not attracted attention due to its narrow range and difficult measurement. Transverse wave velocity as well as longitudinal wave velocity should be measured for nondestructive measurement of Poisson's ratio. Rigid couplants for transverse wave is one of obstacle for scanning over specimen. In the present work, a novel measurement of Poisson's ratio distribution was applied. Immersion method was employed for the scanning over the specimen. Echo signals of normal beam longitudinal wave were collected, and transverse wave modes generated by mode conversion were identified. From transit time of longitudinal and transverse waves, Poisson's ratio was determined without the information of specimen thickness. Poisson's ratio distribution of the carbon steel weldment was mapped. Heat affected zone of the weldment was clearly distinguished from base and filler metals.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2005년도 추계학술발표대회 논문집
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• pp.264-267
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• 2005

Impact damages are very important in the perspective of residual strength of composite structures such as aircrafts, ships, and trains because those damages are sometimes not visible on the surface of the point of impact and the impact resistance of laminated composites is usually not so high. Thus, the impact characteristics of laminated composites should he investigated for the safety of composite structures. This paper investigates the low-velocity impact and damage detection conducted on woven carbon/epoxy laminates. Experimental results show that the type of damage is dependent on the impact energy level and the delamination area becomes larger as the impact energy increases.

• 한국구조물진단유지관리공학회 논문집
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• 제24권6호
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• pp.146-152
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• 2020

본 연구는 강교량의 폐합부재 등 시각적으로 탐지하기 어려운 부위의 강재에 대한 손상을 탐지하기 위한 방법을 개발하기 위한 목적의 기초연구이다. 여러 비파괴 방법들 중에서 초음파 속도법을 활용하여 두께가 다른 시편에 대해서 초음파 속도법을 실시하여, 평균 매질내 전파속도를 도출하였고, 이를 활용하여 강재 부재에 대한 회귀분석을 실시하였다. 동일한 재료일 경우 회귀분석의 결과를 활용하면 다른 부재의 두께를 도출할 수 있을 것으로 예상된다. 또한, 광범위한 범위를 스캐닝하기 위해 200 mm/s로 이동하는 연속스캐닝 기법을 검토하였고, 두께가 변화는 부재의 두께를 효과적으로 예측할 수 있었다.

• 한국전자통신학회논문지
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• 제18권5호
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• pp.965-970
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• 2023

윈드프로파일러와 윈드라이다는 대기경계층에서 시공간 고해상도 바람의 연직분포를 산출한다. 윈드라이다는 DBS(Doppler Beam Swinging)와 VAD(Velocity Azimuth Display) 방법으로 바람 벡터를 산출한다. DBS 방법은 빠른 스캔 시간으로 바람 프로파일을 획득할 수 있다는 장점이 있다. 반면에 연직 빔을 포함한 최소한 두 빔이 필요한 제약이 있어서 자료 수집률 저하의 원인이 된다. 일반적으로 다섯 빔을 사용하는 윈드프로파일러의 자료 수집률을 향상하기 위해 VAD 방식을 개선하였다. 먼저 DBS 방식의 시선속도 자료로 Fourier series를 산출하였다. 방위각 간격을 결정하여 Fourier series로 계산한 시선속도를 VAD 방식에 적용하여 고도별 바람을 산출하였다. DBS 방식으로 바람을 산출하지 못한 고도에서도 바람 벡터를 산출하였고, 두 방식의 결과가 일치하였다.

• 대한의용생체공학회:의공학회지
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• 제7권2호
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• pp.139-146
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• 1986

본 논문은 tms 32010이라는 디지탈 신호 처리용소자를 사용하여 초음하 펄스 도플러 장치를 구현한 것이다. 도플러 장피란 초음파 신호의 송수신 과정에서 발생하는 도플러 효과를 이용하여 혈류의 속도를 측정하는 장치이다. 한 점에서의 속도를 측정하는 단일채널 도플러 장치에서는 실시간 고속 푸리에 변환기를 구현하여 도플러 주하수의 스펙트럼을 측정함으로서 혈류속도를 측정하며 초음파 빔의 일직선상에서의 여러점을 동시에 측정하는 다중채널 도플러 장치에서는 영점교차검출기를 구현하여 평균주파수를 측정하였다. 자중채널 장치는 직렬처리법을 사용하여 하드웨어를 간단히 하였으며 8점에서의 속도를 측정할 수 있도록 하였다.