• Structural Engineering and Mechanics
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• 제59권1호
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• pp.123-132
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• 2016

Many military and commercial aging aircrafts flying beyond their design life may experience severe crack and corrosion damage, and thus lead to catastrophic failures. In this paper, were used in a finite element model to evaluate the effect of corrosion on the adhesive damage in bonded composite repair of aircraft structures. The damage zone theory was implemented in the finite element code in order to achieve this objective. In addition, the effect of the corrosion, on the repair efficiency. Four different patch shapes were chosen to analyze the adhesive damage: rectangular, trapezoidal, circular and elliptical. The modified damage zone theory was implemented in the FE code to evaluate the adhesive damage. The obtained results show that the adhesive damage localized on the level of corrosion and in the sides of patch, and the rectangular patch offers high safety it reduces considerably the risk of the adhesive failure.

• International Journal of Naval Architecture and Ocean Engineering
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• 제6권2호
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• pp.245-256
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• 2014

I-core sandwich panel that has been used more widely is assembled using high power $CO_2$ laser welding. Kim et al. (2013) proposed a circular cone type heat source model for the T-joint laser welding between face plate and core. It can cover the negative defocus which is commonly adopted in T-joint laser welding to provide deeper penetration. In part I, a volumetric heat source model is proposed and it is verified thorough a comparison of melting zone on the cross section with experiment results. The proposed model can be used for heat transfer analysis and thermal elasto-plastic analysis to predict welding deformation that occurs during laser welding. In terms of computational time, since the thermal elasto-plastic analysis using 3D solid elements is quite time consuming, shell element model with multi-layers have been employed instead. However, the conventional layered approach is not appropriate for the application of heat load at T-Joint. This paper, Part II, suggests a new method to arrange different number of layers for face plate and core in order to impose heat load only to the face plate.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2005년도 춘계학술발표대회 논문집
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• pp.240-244
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• 2005

In this study a simple model is developed that predicts impact damage in a composite laminate using an analytical model. The model uses a non-linear approximation method (Rayleigh-Ritz) and the large deflection plate theory to predict the number of failed plies and damage area in a quasi-isotropic composite circular plate (axisymmetric problem) due to a point impact load at its centre. It is assumed that the deformation due to a static transverse load is similar to that occurred in a low velocity impact. It is found that the model, despite its simplicity, is in good agreement with FEM predictions and experimental data for the deflection of the composite plate and gives a good estimate of the number of failed plies due to fibre breakage. The predicted damage zone could be used with a fracture mechanics model developed by the second investigator and co-workers to calculate the compression after impact strength of such laminates. This approach could save significant running time when compared to FEM solutions.

• Journal of Mechanical Science and Technology
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• 제19권4호
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• pp.947-957
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• 2005

In this study a simple model is developed that predicts impact damage in a composite laminate avoiding the need of the time-consuming dynamic finite element method (FEM). The analytical model uses a non-linear approximation method (Rayleigh-Ritz) and the large deflection plate theory to predict the number of failed plies and damage area in a quasi-isotropic composite circular plate (axisymmetric problem) due to a point impact load at its centre. It is assumed that the deformation due to a static transverse load is similar to that oc curred in a low velocity impact. It is found that the model, despite its simplicity, is in good agreement with FEM predictions and experimental data for the deflection of the composite plate and gives a good estimate of the number of failed plies due to fibre breakage. The predicted damage zone could be used with a fracture mechanics model developed by the second investigator and co-workers to calculate the compression after impact strength of such laminates. This approach could save significant running time when compared to FEM solutions.

• 한국전기전자재료학회논문지
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• 제16권12S호
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• pp.1261-1267
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• 2003

Since the grating optical low-pass fillet degrades the resolution of images, we developed a hologram optical low-pass filter that show low degradation of the image and studied its characteristics. We designed the hologram that divides input beam into circular shaped 21 beams with a Monte-Carlo based hologram generation program and calculated its MTE characteristics to compare it with that of a grating filter. The hologram was manufactured through the optical lithography process and attached to a digital imaging device (Zoran 732212) for measurement. The moirfiltering is compared with zone plate images and the resolution loss is measured with USAF resolution chart. The hologram optical low-pass filter showed better characteristics in both moly filtering and resolution.

• International Journal of Naval Architecture and Ocean Engineering
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• 제5권3호
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• pp.348-363
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• 2013

The use of I-Core sandwich panel has increased in cruise ship deck structure since it can provide similar bending strength with conventional stiffened plate while keeping lighter weight and lower web height. However, due to its thin plate thickness, i.e. about 4~6 mm at most, it is assembled by high power $CO_2$ laser welding to minimize the welding deformation. This research proposes a volumetric heat source model for T-joint of the I-Core sandwich panel and a method to use shell element model for a thermal elasto-plastic analysis to predict welding deformation. This paper, Part I, focuses on the heat source model. A circular cone type heat source model is newly suggested in heat transfer analysis to realize similar melting zone with that observed in experiment. An additional suggestion is made to consider negative defocus, which is commonly applied in T-joint laser welding since it can provide deeper penetration than zero defocus. The proposed heat source is also verified through 3D thermal elasto-plastic analysis to compare welding deformation with experimental results. A parametric study for different welding speeds, defocus values, and welding powers is performed to investigate the effect on the melting zone and welding deformation. In Part II, focuses on the proposed method to employ shell element model to predict welding deformation in thermal elasto-plastic analysis instead of solid element model.

• 한국정보통신학회:학술대회논문집
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• 한국해양정보통신학회 2007년도 추계종합학술대회
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• pp.131-134
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• 2007

본 논문에서는 알고리즘의 테스트 패턴중 하나인 1D-CZP패턴의 하드웨어 구현을 제안한다. FPGA를 통한 알고리즘 검증 시 센서로부터 받아들이는 정보로만은 알고리즘의 완벽한 장상작동 유무를 판단하기 어렵기 때문에, 내부 패턴 Generator를 사용하여 센서의 정보와 함께 알고리즘의 정상작동 유무를 판단하게 된다. 본 논문은 필터의 주파수 특성 판단에 용이하며, 입력이 랜덤한 특징을 가지는 1D-CZP패턴을 ROM Table형태로 구현하며, 구현 시 사용되는 Modulus연산을 효율적으로 수정함으로, 하드웨어 사이즈가 작아진 1D-CZP패턴을 제안한다.

• 한국강구조학회 논문집
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• 제29권6호
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• pp.411-422
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• 2017

본 연구에서는 콘크리트피복 원형충전강관 기둥을 적용한 합성구조 접합부의 거동특성과 내진성능을 평가하기 위하여, 기둥-플랜지 접합부에 대한 인장실험과 보-기둥 접합부에 대한 반복하중 실험을 수행하였다. 기둥-플랜지 인장실험은 피복콘크리트의 유무와 플랜지 폭, 인장철근 보강을 변수로 하여 5개의 실험체에 대하여 하중재하능력과 파괴모드를 분석하였다. 실험결과, 접합부에서의 플랜지 단부 폭을 200mm에서 350mm로 증가시킬 경우 연결부의 강도 및 강성이 각각 1.61배와 1.56배가 증가했고, 인장철근을 보강할 경우 추가적으로 강성과 강도가 각각 1.35배와 1.92배 증가했다. 접합부 반복하중 실험에서는 접합 상세를 변수로 3개의 외부접합부 실험체를 구성했다. 접합부 보강상세로는 인장철근 보강과 강관의 두께, 수직강판 보강을 고려하였다. 모든 접합부 실험체는 보에서 뚜렷한 휨항복이 발생하였으며 접합부의 손상은 제한적이었다. 특히, 강재보가 강관에 직접 용접되는 경우 보의 웨브를 통해서도 하중이 전달되기 때문에, 플랜지 인장실험 결과보다 보수적인 설계가 가능하며, 접합부 강관 두께를 증가시키거나 수직강판으로 보강한 경우에는 추가적으로 패널존의 전단내력이 증가하는 것으로 나타났다.

• 한국임상수의학회지
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• 제26권6호
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• pp.586-590
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• 2009

철선충은 주로 사마귀와 같은 곤충에 기생하는 선충류로 사람이나 동물은 우연히 감염될 수 있는 것으로 알려져 왔다. 철선충의 생활사는 크게 곤충에 기생하는 기생생활기, 그리고 발육이 완료된 후에 숙주를 죽이고 외계로 나와 자유생활을 하는 자유생활기로 구분할 수 있다. 본 연구는 개의 구토물에서 오디흑연가시 수컷을 발견하여 이의 횡단면을 주사 및 투과 전자현미경으로 관찰한 것이다. 전자현미경하에서 표피는 4층(epicuticle, cuticle, epidermis, muscle)으로 이루어졌고, 내강에는 장, 배신경절이 발견되었다. 그러나 고환은 발견되지 않았다. 표피의 최상층에서 여러 형태의 areoles이 관찰되었으며, cuticle은 17열의 섬유로 이루어져 있었다. Epidermis는 1열로 구성되어 있었으며, muscle층은 여러 개의 근세포가 종으로 일정하게 배열되어 있었다. 그리고 내강에 배신경절이 충체의 정중앙 배측에서만 존재하는 것으로 확인되었다. 이러한 결과로 본 철선충은 기생생활기를 끝내지 못한 미성숙충으로 판단된다.