• Proceedings of the KSME Conference
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• 2005.11a
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• pp.129.1-129.1
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• 2005

• Proceedings of the Korean Geotechical Society Conference
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• 2001.03a
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• pp.57-64
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• 2001

암석-콘크리트 불연속면의 전단변형 및 파괴특성을 규명하기 위해 상부 재료를 콘크리트로, 하부 재료를 암석으로 하는 규칙.불규칙 톱니형 시료와 인공 절리시료를 제작하여 실험실 직접전단시험을 실시하였다. 전단과정 동안 하중과 변위 외에 미소파괴음의 계수와 에너지를 측정하여 전단과정의 단계별 특징을 규명하였고 미소파괴음 음원추적을 실시하여 불연속면에서의 거칠기 파괴부분의 변화를 고찰하였다. 또한 암석 불연속면과 암석-콘크리트 불연속면의 거동을 비교하고 거칠기의 불규칙성 증가에 따른 전단거동의 변화를 관찰하였다.

• Proceedings of the Korean Nuclear Society Conference
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• 1998.05b
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• pp.48-53
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• 1998

원자력 발전소 배관계통에 파단전 누설 (LBB) 설계개념의 적용을 위해서는 원자로 가동온도에서의 재료의 파괴저항성 평가가 필수적이다. 본 연구에서는 국내 원자로의 1차 냉각계통배관의 엘보우 소재로 사용되는 SA516-Gr.70 강의 파괴저항성에 미치는 DSA (Dynamic Strain Aging, 동적변형시효) 영향을 고찰하였다. 파괴저항성 평가를 위해 원자로 가동온도를 포함한 상온~50$0^{\circ}C$ 온도영역에서 준정적 하중에서부터 지진 하중 정도의 동적 하중까지 하중속도를 달리하여 직류전위차법 (DCPD) 이용하여 J-R 시험을 행하였다. J-R 시험결과, SA516-Gr.70 강은 특정한 온도와 하중속도의 조합에서 파괴저항성이 크게 떨어지는 양상을 보였으며, 낮은 파괴저항성을 나타내는 온도는 하중속도가 증가함에 따라 높은 온도쪽으로 이동하는 전형적인 DSA 감수성을 보였다. 인장시험을 통해서도 큰 폭의 serration 이 관찰되었으며 SA516-Gr.70 강에서 파괴저항성의 변화와 DSA 현상과의 연관성을 고찰하였다.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.37 no.4
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• pp.491-496
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• 2013

Finite element simulations of tensile tests were performed to determine the equivalent stress - equivalent plastic strain curves, critical equivalent stresses, and critical equivalent plastic strains. Then, the curves were used as inputs to finite element simulations of fracture toughness tests to determine the plane strain fracture toughness. The critical COD was taken as the COD when the equivalent plastic strain at the crack tip reached a critical value, and it was used as a crack growth criterion. The relationship between the critical COD and the critical equivalent plastic strain or the reduction of area was found. The relationship between the plane strain fracture toughness and the product of the critical equivalent stress and the critical equivalent plastic strain was also found.

• Proceedings of the KIEE Conference
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• 2000.07c
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• pp.1575-1577
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• 2000

345kV급 210KN 초고압 현수애자의 개발 시험 결과, 과전파괴하중시험에서 품질관리지수가 3.0 이상인 11.2였으며, 유중파괴전압시험에서는 기준치보다 40% 정도 높은 값을 보였다. 그리고 72kA$\cdot$ Cycle $\pm$10% 조건의 power arc시험에 파괴없이 만족하였으며, 경년변화시험 후의 확인시험에서도 품질관리지수가 11.47로 높게 나타났다. 애자련의 피로시험 및 진동피로시험 후의 하중확인시험에서도 기준치보다 10% 이상의 값을 보였다. 전체적인 시험조건에서 경년변화시험의 조건이 가장 가혹한 것으로 나타났다.

• Aerospace Engineering and Technology
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• v.6 no.1
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• pp.230-236
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• 2007

The quality control of composite structure includes inspection, testing and monitoring in all processes from receiving inspection to part fabrication. The purpose of these activities is to ensure that the design objectives are consistently achieved. The quality factors include material, receiving inspection, storage and shelf-life control, environmental control, testing, inspection and record control. This paper presents the process verification method using destructive test and quality control method in composite structure of aircraft. And it is believed that the destructive test will be basis to obtain a reliability of non-destructive test in complex composite structure and to ensure the design requirements in composite part.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.36 no.7
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• pp.769-776
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• 2012

The damage analysis method in this paper needs a material property and failure criteria. The material properties and the failure criteria could be easily obtained from the results of notched bar tensile tests carried out on other materials studied previously. However, for the cast stainless steel (CF8M) material in this paper, because of the variance in the results from notched bar tensile tests under the same conditions, the material property and the failure criteria could be obtained differently, depending on the analyzer. Therefore, a proper procedure that can confirm the material property and failure criteria are needed. In this work, the averaged material property was obtained from the notched bar with a 16-mm notch radius, and three failure criteria for CF8M material by finite element analysis were obtained. Applying the material property and the failure criteria, FE damage analysis for the J-R fracture toughness test was conducted. For validation, the simulated results were compared with the experimental results.

• Journal of the Korean Society for Nondestructive Testing
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• v.21 no.3
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• pp.251-260
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• 2001

Damage Profess of CFRP laminates under monotonic tensile test was characterized by the correlation between Acoustic Emission(AE) and Ultrasonic Test(UT). The amplitude distribution of AE signal from a specimens is an aid to the determination of the extent of the different fracture mechanism such as matrix crack, debonding, fiber pullout and fiber fracture as load is increased. In addtion, the characteristics of ultrasonic amplitude attenuation are useful lot analysis of the different type of fracture mechanism. Different orientation of carbon fiber reinforced plastic specimens were used to investigate the AE amplitude range and ultrasonic amplitude attenuation. Finally, loading-unloading tests were carried out to check Felicity effect. During the tests, ultrasonic amplitude attenuation was investigated at the same time and compared with AE parameters. The result showed that two parameters of both AE and UT could be effectively used for analysis of fracture mechanism in CFRP laminates.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.10 no.4
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• pp.1-10
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• 1990

RILEM proposed three point bend test to determine the fracture energy of concrete, but there is discrepancy between the theoritical and the experimental fracture energy of concrete by the influence of self-weight of concrete. This paper presents four point bend test using proving ring in order to take into account the influence of self-weight of concrete. The initial notch to beam depth ratio was varied from 0.2 to 0.6 in order to investigate the variation of fracture energy of concrete according to the variation of initial notch depth. The proposed four point bend test using proving ring was verified to be superior to three point bend test.

• Composites Research
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• v.13 no.4
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• pp.54-66
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• 2000

Interfacial and microfailure properties of carbon fiber/epoxy matrix composites were evaluated using both tensile fragmentation and compressive Broutman tests with an aid of acoustic emission (AE) monitoring. A polymeric maleic anhydride coupling agent and a monomeric amino-silane coupling agent were used via the electrodeposition (ED) and the dipping applications, respectively. Both coupling agents exhibited significant improvements in interfacial shear strength (IFSS) compared to the untreated case under tensile and compressive tests. The typical microfailure modes including fiber break of cone-shape, matrix cracking, and partial interlayer failure were observed during tensile test, whereas the diagonal slippage in fiber ends was observed under compressive test. For both loading types, fiber breaks occurred around just before and after yielding point. In both the untreated and treated cases AE amplitudes were separately distributed for the tensile testing, whereas they were closely distributed for the compressive tests. It is because of the difference in failure energies of carbon fiber between tensile and compressive loading. The maximum AE voltage for the waveform of carbon or basalt fiber breakages under tensile tests exhibited much larger than those under compressive tests, which can provide the difference in the failure energy of the individual failure processes.