• Journal of Biosystems Engineering
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• 제18권1호
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• pp.15-20
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• 1993

Wearness has been a major failure criterion in Korean-made rotary blade. However, few studies have been conducted to improve it. In this study, the fundamental data obtained from the measurement of wearness and failure of rotary blade were analyzed to provide a guideline for the design of rotary blades. For the straight part(about 20-23 em from bolt hole) from the bolt hole to bending point of rotary blade, modifications were proposed for improvements, however, for the portion from bending point to tip was made no design recommendations because the failure behavior of that portion was difficult to analyze with the experimental data. The results are summarized as follows. 1. The current V-shape section has to be moved about 5 em toward the bending point of rotary blade. 2. The section modulus at the portion about 5-7 em distant from bolt hole has to be increased about 15-20 %. 3. The V-shape section has to be changed into U-shape to reduce the on account of recieving initial stress in blades. 4. The radius of curvature of the neck(the portion about 5-7 cm apart from bolt hole) has to be made larger to decrease the stress concentration.

• Structural Engineering and Mechanics
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• 제74권1호
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• pp.19-32
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• 2020

Metallic energy-dissipation dampers are widely used in structures. They are comprised of an added damping and stiffness (ADAS) device with many parallel, diamond-shaped hole plates, the neck width of which is an important parameter. However, no studies have analyzed the neck width's influence on the ADAS device's performance. This study aims to better understand that influence by conducting a pseudo-static test on ADAS, with three different neck widths, and performing finite element analysis (FEA) models. Based on the FEA results and mechanical theory, a design neck width range was proposed. The results showed that when the neck width was within the specified range, the diamond-shaped hole plate achieved an ideal yield state with minimal stress concentration, where the ADAS had an optimal energy dissipation performance and the brittle shear fracture on the neck was avoided. The theoretical values of the ADAS yield loads were in good agreement with the test values. While the theoretical value of the elastic stiffness was lower than the test value, the discrepancy could be reduced with the proposed modified coefficient.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2004년도 춘계학술대회
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• pp.7-12
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• 2004

Large-sized pins are usually used to lift and handle large low speed diesel engine crankshaft. There has then been a need to reduce and optimize the weight of the traditionally used pins. Making an hole by cutting the inside of the pin out was investigated in view of static and fracture strength. To compensate the stress increase caused by the introduction of the inner hole, the groove in the circumferential direction pre-existing on the pin is to be removed. Finite element analysis was carried out for both the original model and weight reduced model. Stress intensity factors for semi-elliptical defects assumed on the pin for the original model and weight reduced model was calculated using the ASME method and compared with the fracture toughness test result of the pin material. The diameter of the cutting hole for the revised model was determined based on the analysis results.

• Structural Engineering and Mechanics
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• 제60권6호
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• pp.939-952
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• 2016

A compression to tensile load transforming (CTT) device was developed to determine indirect tensile strength of concrete material. Before CTT test, Particle flow code was used for the determination of the standard dimension of physical samples. Four numerical models with different dimensions were made and were subjected to tensile loading. The geometry of the model with ideal failure pattern was selected for physical sample preparation. A concrete slab with dimensions of $15{\times}19{\times}6cm$ and a hole at its center was prepared and subjected to tensile loading using this special loading device. The ratio of hole diameter to sample width was 0.5. The samples were made from a mixture of water, fine sand and cement with a ratio of 1-0.5-1, respectively. A 30-ton hydraulic jack with a load cell applied compressive loading to CTT with the compressive pressure rate of 0.02 MPa per second. The compressive loading was converted to tensile stress on the sample because of the overall test design. A numerical modeling was also done to analyze the effect of the hole diameter on stress concentrations of the hole side along its horizontal axis to provide a suitable criterion for determining the real tensile strength of concrete. Concurrent with indirect tensile test, the Brazilian test was performed to compare the results from two methods and also to perform numerical calibration. The numerical modeling shows that the models have tensile failure in the sides of the hole along the horizontal axis before any failure under shear loading. Also the stress concentration at the edge of the hole was 1.4 times more than the applied stress registered by the machine. Experimental Results showed that, the indirect tensile strength was clearly lower than the Brazilian test strength.

• Composites Research
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• 제18권6호
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• pp.9-18
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• 2005

복합재료가 항공기 구조물 및 기계부품 등에 폭 넓게 적용됨에 따라, 복합재료 구조물에서 가장 취약한 복합재료 체결부의 설계는 매우 중요한 연구 분야로 대두되고 있다. 본 논문에서는 기계적으로 체결이 된 단일 및 다중 핀 하중을 받는 복합재료 평판에서 응력분포에 대한 해석적인 연구를 수행하였다. 또한, 기계적체결부인 핀과 구멍간에서 접촉 문제를 다루기 위하여 접촉응력해석을 이용한 유한요소 모델이 사용되었으며, 응력분포를 정량적으로 비교하기 위하여 무차원화한 응력집중계수를 이용하였다. 단일 핀 하중을 받는 경우에 대하여 적층순서, 원공의 지름에 대한 평판 폭의 비 (W/D ratio), 원공의 지름에 대한 끝단에서 원공까지의 길이의 비 (En ratio), 마찰계수, 와셔의 조임력 등에 대한 영향을 알아보았으며, 다중 핀 하중을 받는 경우에 응력집중계수를 이용하여 핀의 개수, 피치, 열의 개수, 열 간격 및 원공의 배치형상의 영향에 대하여 알아보았다. 단일 핀 하중을 받는 경우에 대한 결과로부터, DBLT (Double-Bias-Longitudinal Transverse) 복합재료 평판에서 응력이 가장 민감하게 나타나는 것을 알 수 있었고, 원공의 지름에 대한 평판 폭의 비와끝단에서 원공까지의 길이의 비에 따른 응력의 변화가 민감하게 나타나는 것을 확인할 수 있었다. 또한, 다중핀 하중을 받는 경우에 대한 응력해석의 결과로부터, 원공이 2열로 배치된 복합재료 평판에서 응력집중현상이 가장 적게 일어나는 것을 확인하였다. 이러한 해석을 통하여, 체결부에서 나타나는 응력분포로부터 복합재료 평판에서의 파손형태를 예측할 수 있다.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2002년도 추계학술발표대회 논문집
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• pp.88-91
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• 2002

The two dimensional size effect of specimen gauge section (length x width) was investigated on the compressive behavior of a T300/924 [45/-45/0/90]3s, carbon fiber-epoxy laminate. A modified ICSTM compression test fixture was used together with an anti-buckling device to test 3mm thick specimens with a 30$\times$30, 50$\times$50, 70$\times$70, and 90mm$\times$90mm gauge length by width section. In all cases failure was sudden and occurred mainly within the gauge length. Post failure examination suggests that $0^{\circ}$ fiber microbuckling is the critical damage mechanism that causes final failure. This is the matrix dominated failure mode and its triggering depends very much on initial fiber waviness. It is suggested that manufacturing process and quality may play a significant role in determining the compressive strength. When the anti-buckling device was used on specimens, it was showed that the compressive strength with the device was slightly greater than that without the device due to surface friction between the specimen and the device by pretoque in bolts of the device. In the analysis result on influence of the anti-buckling device using the finite element method, it was found that the compressive strength with the anti-buckling device by loaded bolts was about 7% higher than actual compressive strength. Additionally, compressive tests on specimen with an open hole were performed. The local stress concentration arising from the hole dominates the strength of the laminate rather than the stresses in the bulk of the material. It is observed that the remote failure stress decreases with increasing hole size and specimen width but is generally well above the value one might predict from the elastic stress concentration factor. This suggests that the material is not ideally brittle and some stress relief occurs around the hole. X-ray radiography reveals that damage in the form of fiber microbuckling and delamination initiates at the edge of the hole at approximately 80% of the failure load and extends stably under increasing load before becoming unstable at a critical length of 2-3mm (depends on specimen geometry). This damage growth and failure are analysed by a linear cohesive zone model. Using the independently measured laminate parameters of unnotched compressive strength and in-plane fracture toughness the model predicts successfully the notched strength as a function of hole size and width.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2002년도 추계학술대회 논문집
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• pp.833-836
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• 2002

Sometimes open holes are required for the function and the weight reduction of structure and machinery. However, the serious stress concentration occurs because of the geometric discontinuity caused by the holes and cutting section. In this study, it is attempted to obtain the stress concentration coefficients of the inner surface of the hole boundary by changing the position and the shape of holes on the homogeneous isotropic plate. And the effects on the plate are investigated. The results show that the stress level becomes low and the distribution area widens the position of stress concentration changes as the ratio ah increases and change to a circle. And as the ratio a/l decreases, the stress concentration reduces.

• The Korean Journal of Ceramics
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• 제6권2호
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• pp.150-154
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• 2000

Mobilities of electrons ($\mu_p$) and holes ($\mu_p$) in 2, 5, and 10 mol% $TiO_2$-doped yttria stabilized zirconia (TD-YSZ) have been estimated by a non-steady state gas permeation method using models proposed by Weppner and Maruyama. Values of $\mu_n$ and $\mu_p$ were found to be closed to those in non-doped YSZ reported earlier. The concentration of electrons and holes were calculated from $\mu_n$ and $\mu_p$ values and the partial conductivities of electrons and holes measured by a dc-polarization method. The concentration of electrons at unit oxygen partial pressure increased with increasing $TiO_2$concentration, while the hole concentration was almost independent of $TiO_2$concentration.

• Composites Research
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• 제24권4호
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• pp.29-35
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• 2011

전통적인 특성길이 방법을 이용하여 원공이 있는 복합재 적층판의 강도를 예측하기 위해서는 원공이 있는 적층뿐만 아니라 원공이 없는 적층판에 대한 시험 결과와 유한요소해석이 필요하였다. 본 논문에서는 응력집중계수와 재료상수를 이용하여 유한요소해석 없이 복합재 적층판 원공 주위의 응력분포 및 인장특성길이를 추정하고, 이를 바탕으로 원공이 있는 복합재 적층판의 인장강도를 예측할 수 있는 방법을 제안하였다. 또한 새로운 방법에서는 재료의 효과가 변수로 고려되므로 다양한 재료에 대한 적용이 가능하며 원공이 있는 복합재 적층판에 대한 시험도 생략할 수 있다. 적층판 주위의 응력분포는 유한요소해석과의 비교를 통해 검증하였고, 최종적으로는 USN125 탄소/에폭시 적층판을 제작하여 파손하중 예측 결과와 시험 결과를 비교하였다. 원공이 있는 다양한 형상의 복합재 적층판의 파손강도 예측 결과는 최대 8% 이내의 오차로 시험 결과와 잘 일치함을 확인하였다.

• 터널과지하공간
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• 제26권5호
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• pp.409-417
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• 2016

본 전통석유자원을 대체할 수 있는 석유자원으로 부상하고 있는 셰일가스가 부존된 셰일층은 낮은 투과성을 가지고 있어 생산성을 향상시키기 위해 수압파쇄법이 적용된다. 본 연구는 일반 시추공과 나선형 홈을 가지는 시추공을 모사한 축소 모형 시험체에 대해 실내수압파쇄 시험을 실행하고 초기파쇄압과 유체접촉상태를 비교 분석하여 공벽형상에 따른 수압파쇄결과를 알아보았다. 또 그 결과를 3차원 개별요소 프로그램인 3DEC을 이용한 수치해석 모델링 값과 비교하였으며, 선행연구 자료와 비교하여 신뢰성 있는 결과를 도출하고자 하였다. 실험결과 고압수의 접촉면적보다는 유도홈의 형태에 의한 응력집중의 효과가 수압파쇄에 더욱 효율적이였다. 따라서 고압수의 응력집중을 높일 수 있는 인공적인 유도홈을 만들 시 적은 수압으로 큰 파쇄효과를 나타낼 수 있을것으로 생각된다.