• 터널과지하공간
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• 제21권4호
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• pp.307-319
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• 2011

교통, 굴착, 발파 등에 의한 반복하중은 오랜 시간에 걸쳐서 암석의 미세균열 성장을 일으키며, 암석의 강도 등에 영향을 미치기 때문에 반복하중에 의한 균열의 성장, 결합은 장시간 안정성 평가에 중요한 영향을 미친다. 본 연구에서는 두 개의 초기 균열을 가지는 모사 암석 시험편에 단조증가 및 반복하중을 가하여 하중 조건에 따른 균열의 성장과 결합유형을 조사하였다. 단조증가하중, 반복하중 시험 모두에서 서로 유사한 날개균열 시작 위치, 날개균열 각도, 균열 성장 순서, 균열 결합 형태가 관측되었다. 본 연구에서 관찰된 균열 결합은 크게 3종류로 전단에 의한 결합, 1개의 날개 혹은 인장 균열에 의한 결합 그리고 2개의 날개 혹은 인장 균열에 의한 결합으로 요약될 수 있다. 피로균열은 반복하중 시험에서만 발생하였으며 성장 방향은 이차균열과 유사하게 초기균열과 같은 방향 혹은 하중방향과 직교인 수평방향으로 관찰되었다.

• 열처리공학회지
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• 제14권4호
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• pp.212-219
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• 2001

The fatigue test was carried out to evaluate the fatigue characteristics of fire resistance steel for frame structure and heat affected zone (HAZ) by the one side Gas Metal Arc Welding (GMAW). In this paper, the fatigue crack growth behavior was investigated with the compact tension specimen of base metal and the HAZ according to chemical composition and rolling end temperature, respectively. And the acoustic emission signals obtained from the fatigue test were analyzed by the time-frequency analysis method as a nondestructive evaluation. Main results obtained are summarized as follows; The hardness was appeared softening phenomenon that weld metal and HAZ are lower than that of base metal. Fatigue life of welded specimen was longer than that of base metal. m was 3~4.5 in base metal and 3.8~5.8 in HAZ. The main frequency range of acoustic emission signal analyzed from time-frequency method is different with the range by noise and crack. Also, it could be classified that it was also generated by fracture mechanics of dimple, inclusion etc.

• 한국콘크리트학회:학술대회논문집
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• 한국콘크리트학회 1999년도 봄 학술발표회 논문집(I)
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• pp.793-798
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• 1999

This study was conducted to evaluate structural integrity and crack source location of plain concrete beams using acoustic emission. Three point bending tests were carried out plain concrete specimen under cyclic loadings. The variable is W/C of concrete. From the tests it was shown that a breakdown of the kaiser effect and high AE activities during unloading could be effective indices to estimate the level of deterioration in plain concrete structures. The time and location and propagation of crack could be easily determined by monitoring AE, which concludes that AE technique can be a very useful tool to evaluate structural integrity of concrete plain beams.

• 한국기계가공학회지
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• 제6권3호
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• pp.92-97
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• 2007

The overlay welding the automobile where the durability is demanded, it is used in the vessel engine valve, plant valve and pump parts. Cause of damage public opinion one what is thought is the fatigue load due to the opening and shutting operation right time repetition of the engine valve. The damage cause of the engine valve or explanation of destruction mechanism is very difficult. The research which it sees to make clear a overlay welding of Co-alloy by Plasma Transferred Arc Weld Surfacing Process reconsideration fatigue crack initiation and fatigue crack growth mechanism at high temperature.

• 대한기계학회논문집A
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• 제39권12호
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• pp.1281-1286
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• 2015

항공기는 다양한 임무를 수행함으로써 장기간 운영 시 비행시간 누적으로 인해 피로균열을 발생시킬 수 있다. 주익 구조물에 균열이 발생하면 수명단축 등 여러 문제점들이 발생할 수 있다. 이의 해결을 위해 피로임계위치(Fatigue critical location, FCL)에서의 균열진전 해석이 필요하다. 균열진전 해석을 위해서는 장시간의 응력 스펙트럼이 필요한데 실제 항공기에서 필요한 만큼의 데이터를 얻는 것은 막대한 시간과 비이 소요된다. 본 논문에서는 SwRI(South West Research Institute)보고서에 제시되어있는 임무별 단시간 하중배수 자료를 바탕으로 Peak-Valley Cycle Counting 을 진행하여 장시간의 응력 스펙트럼을 산출하는 알고리즘을 개발하였다.

• 콘크리트학회논문집
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• 제18권4호
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• pp.543-552
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• 2006

사용성 한계상태로서의 균열폭 예측에 관한 현재의 교량설계 시방기준은, 부식의 시작과 진행에 의한 균열폭을 고려할 때 이론적으로 불충분하다. 균열폭은 하중, 부착, 미끄러짐, 그리고 철근이나 긴장재의 부식에 영향을 받게 된다. 콘크리트 교량의 생애주기 동안의 시간 의존적 일반부식을 고려하여, 균열폭 예측식을 제안하였다. 개발된 부식모델과 균열예측식은 프리스트레스트 콘크리트교량과 일반콘크리트교량의 설계시 시간단계별로 물-시멘트 비, 피복두께, 단면형상의 변화에 따른 극한한계상태와 사용성한계상태의 평가에 사용될 수 있다. 또한 기존교량의 시간단계별 극한 한계상태 및 사용성한계 상태의 평가를 통해서 정량적인 유지관리 및 잔존수명예측에 기여할 것으로 기대한다.

• 한국자동차공학회논문집
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• 제12권1호
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• pp.196-202
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• 2004

The development of new materials with light weight and high strength has become vital to the machinery, aircraft and auto industries. However, there are a lot of problems with developing such materials that require expensive tools, and a great deal of time and effort. Therefore, the improvement of fatigue strength and fatigue life are mainly focused on adopting residual stress(in this thesis). The compressive residual stress was imposed on the surface according to each shot velocity(57, 70, 83, 96 m/sec) based on Shot-peening, which is the method of improving fatigue life and strength. By using the methods mentioned above, the following conclusions have been drawn. 1. The fatigue crack growth rate(da/dN) of the Shot-peened material was lower than that of the Un-peened material. And in stage I, ΔKth, the threshold stress intensity factor, of the shot-peen processed material is high in critical parts unlike the Un-peened material. Also m, fatigue crack growth exponent and number of cycle of the Shot-peened material was higher than that of the Un-peened material. That is concluded from effect of da/dN. 2. Fatigue life shows more improvement in the Shot-peened material than in the Un-peened material. And compressive residual stress of surface on the Shot-peen processed operate resistance force of fatigue crack propagation.

• 대한기계학회논문집
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• 제18권5호
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• pp.1134-1143
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• 1994

A study of adiabatic shear band formation and propagation of 4340 steel was done using the stepped speciment which was subjected to high velocity impact. The high velocity impact was performed on compression Hopkinson bar impact machine. After the controlled impact, the specimen was prepared for visual inspection. Numerical simulation was also performed with same geometrical dimension using explicit time integration finite element code. Experimental results were then compared with the numerical prediction. It was found that the numerical prediction is quite accurate, average thickness of adiabatic shear band is about $10{\mu}m$, the macro crack around shoulder is due to folding, and the deformation control ring is effective to freeze the propagation of adiabatic shear band.

• Structural Engineering and Mechanics
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• 제74권3호
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• pp.313-323
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• 2020

Non-destructive tests are commonly used in construction industry to access the quality and strength of concrete. However, till date there is no non-destructive testing method that can be adopted to evaluate the bond condition of reinforced concrete beams. In this regard, the presented research work details the use of ultra-sonic pulse velocity test method to evaluate the bond condition of reinforced concrete beam. A detailed experimental research was conducted by testing four identical reinforced concrete beam samples. The samples were loaded in equal increments till failure and ultra-sonic pulse velocity readings were recorded along the length of the beam element. It was observed from experimentation that as the cracks developed in the sample, the ultra-sonic wave velocity reduced for the same path length. This reduction in wave velocity was used to identify the initiation, development and propagation of internal micro-cracks along the length of reinforcement. Using the developed experimental methodology, researchers were able to identify weak spots in bond along the length of the specimen. The proposed method can be adopted by engineers to access the quality of bond for steel reinforcement in beam members. This allows engineers to carryout localized repairs thereby resulting in reduction of time, cost and labor needed for strengthening. Furthermore, the methodology to apply the proposed technique in real-world along with various challenges associated with its application have also been highlighted.

• Advances in concrete construction
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• 제7권1호
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• pp.39-50
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• 2019

This study presents a comprehensive experimental investigation on mostly encountered types of Reinforced Concrete Haunched Beams (RCHBs) where three modes of RCHBs investigated; the diversity of studied beams makes it a pioneer in this topic. The experimental study consists of twenty RCHBs and four prismatic beams. Effects of important parameters including beam type, the inclination angle, flexure and compressive reinforcement, shear reinforcement on mechanical behavior and failure mode of each mode of RCHBs were examined in detail. Furthermore crack propagation at certain load levels were inspected and visualized for each RCHB mode. The results confirm that RCHBs have different behavior in shear as compared to the prismatic beams. At the same time, different mechanical behavior was observed between the modes of RCHBs. Therefore, RCHBs were classified into three modes according to the inclination shape and mode of failure (Modes A, B and C). However, it was observed that there is no significant difference between RCHBs and prismatic beams regarding flexural behavior. Moreover, a new and unified formula was proposed to predict the critical effective depth of all modes of RCHBs that is very useful to predict the critical section for failure.