• 한국정밀공학회지
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• 제20권2호
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• pp.129-135
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• 2003

The fatigue life of a structure can be enhanced by improving the mechanical and metallurgical aspects to strengthen the material around regions of high stress. Coldworking of holes in structures is one of the mechanical methods of strengthening material. The material for this research is A12024-T351 which is used for the primary member or aircraft. Specimens were tested under constant amplitude loading and residual stresses measured by X-ray diffraction technique. Fatigue crack initiation life was evaluated by a strain-life equation which was considered initial residual stress and residual stress relaxation exponent as a function of the strain amplitude. The predictions on fatigue crack initiation life were compared with experimental results. A wide range of discrepancies between them was found.

• 한국지반공학회지:지반
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• 제11권1호
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• pp.113-126
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• 1995

점성토의 변형특성을 연구하기 위하여 공진주(RC)시험과 비틀전단(75)시험을 저변형률 및 중간 변형률하에서 실시하여 변형률의 크기,진동주파수,하중반복회수의 영향을 살펴보았다. 소 성지수가 이들의 영향을 평가하는데 중요한 변수임을 알 수 있었다. 실험에 사용된 시료로는 불 교란 실트 및 점토와 실험실에서 다져진 노상토를 사용하였다. 선형한계변형률이하에서 전단탄 성계수는 하중반복회수와 변형률의 크기에 영향을 받지 않았으며, RC시험에서 얻은 최소감소비가 1.1%에서 1.7%영역에서 존재하였다. 점성토의 선형한계변형률은 구속압과 소성지수에 따라 증가하였으며 사질토와 비교하여 넘은 선형영역을 보였다. 반복한계변형률이상의 변형률하에서는 전단탄성계수는 하중반복회수에 따라 감소하였지만 감쇠비는 영향을 받지 않았다. 진동주파수의 영향에 의해 RC시험에서 얻은 점성토의 전단탄성계수와 감쇠비는 RC시험결과보다 컸다. 전단탄성계수는 진동주파수의 대수증가에 따라 선형적으로 증가하였고 감쇠비의 경우 2Hz이하의 저주파수영역에서는 영향을 받지 않았다.

• 한국지반공학회지:지반
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• 제10권2호
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• pp.85-96
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• 1994

공진주 실험기는 전단탄성계수, 영계수 및 감쇠비로 표현되는 지반의 동적물성치를 연구하기 위한 중요한 실내 실험법으로 널리 사용되어 왔다. 본 연구에서는 Stokoe식 공진주 실험기를 이용하여 전단 변형률 10-4%-10-1% 범위에서 대표적인 국내 노상토의 동적 물성치를 연구하였다. 전단탄성계수와 감쇠비는 한계변형률 Ix10-3%부근에서 부터 변형률의 영향을 받기 시작 하였다. 한계 변형률 이하에서 최대 전단탄성계수(Gmin)는 구속압 (Qc)에 따라 (Qc)0.61에 비례하여 증가하였고 최소감쇠 비(Dmin)는 1%-5.7% 범위에 분포하였다. 한계 변형률 이상에서 정규화 탄성계수 감소곡선은 Ramberg-Osgood식으로 잘 나타낼 수 있으며 Seed와 Idriss가 사질토 를 이용하여 얻은 감소곡선과 거의 일치하였다.

• 한국지반공학회:학술대회논문집
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• 한국지반공학회 1998년도 가을 학술발표회 논문집
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• pp.461-468
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• 1998

• 한국지진공학회논문집
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• 제2권4호
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• pp.53-62
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• 1998

구조물의 내진 성능 향상을 위해 현재 종종 사용되어지고 있는 기초분리장치인 적층고베어링과 납-고무 베어링의 내진성능을 실험적으로 파악하였다 베어링의 전단 변형률 또는 가해진 수직 하중이 클수록 베어링의 전단 강성은 감소하며 가력 속도에 대한 영향을 무시할 만하다. 베어링은 순수압축력에는 강하며 인장력에는 그 반대이다.

• International Journal of Aeronautical and Space Sciences
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• 제7권1호
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• pp.137-147
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• 2006

In this study, shape memory alloy damper with characteristics of pseudoelastic hysteresis for helicopter rotor blades are investigated. SMAs can be available in damping augmentation of vibrating structures. SMAs show large hysteresis in the process of pseudoelastic austenite-martensite phase transformation which takes place while subjected to loading above the austenite finish temperature. Since SMAs display pseudoelastic hysteresis behavior over large strain ranges, a significant amount of energy dissipation is possible. A damper can be designed with SMA wires prestressed to a baseline level somewhere in the middle of the pseudoelastic stress range. An experimental study of the effects of pre-strain and cyclic strain amplitude as well as frequency on the damping behavior of pseudoelastic shape memory alloy wires are performed. The effects of the shape memory alloy damper on aeroelastic and ground resonance stability of helicopter are studied. In aeroelastic stability, the dynamic characteristics of blades related to pitch angle and the amplitude of lag motion for the rotor equipped with SMA damper were examined. The performance of SMA damper on ground resonance instability are presented through the frequencies and modal damping with respect to rotating speed.

• 전자공학회논문지D
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• 제35D권1호
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• pp.79-83
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• 1998

We analyzed dynamic-strain perturbations applied to a fiber Bragg grating. The fiber Mach-Zehnder interferometer was used, and by analyzing the interference signal wecould obtain the frequency and relative amplitude information of the dynamic-perturbation. The minimum detectable dynamic-strain using the system was ~9.5 nstrain RMS/.root.(Hz) at 500 Hz. Also we proposed and demonstrated a new method which uses a temperature-discriminating dual-trating sensor head. With the method, we could measure the dynamic -strain as well as static-static-strain even for the case in which the optical pathe difference modulation was applied.

• 한국철도학회논문집
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• 제7권2호
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• pp.85-92
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• 2004

This paper consists of two parts. One is finite element analysis of the redistribution of residual stresses of weld specimen by cutting. This work is necessary to predict the actual residual stress distribution of weld specimens used in fatigue test. The other subject is to calculate the relaxation of residual stress and the strain field induced by cyclic loading. To obtain fatigue life of weldment, the value of strain amplitude at each position is necessary, for example in the strain-life approach, and the numerical results can be used to verify experimental strain measurements. Thermo mechanical finite element analyses were conducted on the commercial package ABAQUS.

• 소성∙가공
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• 제19권1호
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• pp.11-16
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• 2010

The influence of pre-strain on low cycle fatigue behavior of Fe-18Mn-0.05Al-0.6C TWIP steel was studied by conducting axial strain-controlled tests. As-received plates were deformed by rolling with reduction ratios of 10 and 30%, respectively. A triangular waveform with a constant frequency of 1 Hz was employed for low cycle fatigue test at the total strain amplitudes in the range of ${\pm}0.4\;{\sim}\;{\pm}0.6$ pct. The results showed that low-cycle fatigue life was strongly dependent on the amount of pre-strain as well as the strain amplitude. Increasing the amount of prestrain, the number of reversals to failure was significantly decreased at high strain amplitudes, but the effect was negligible at low strain amplitudes. A new model for predicting fatigue life of pre-strained body has been suggested by adding ${\Delta}E_{pre-strain}$ to the energy-based fatigue damage parameter. Also, high-cycle fatigue lives predicted using the low-cycle fatigue data well agreed with the experimental ones.

• 대한기계학회논문집A
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• 제27권1호
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• pp.167-174
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• 2003

Fatigue damage of 2.2Ni-1Cr-0.5Mo steel used fir high strength pressure tubes and vessels was evaluated using uniaxial specimens subjected to strain-controlled fatigue loading. Based on the fatigue test results from different strain ratios of -2. -i 0, 0.5, 0.75, the fatigue damage of the steel was represented by using a cyclic strain energy density. Mean stress relaxation depended on the magnitude of the applied strain amplitude. The high pressure vessel steel exhibited the cyclic softening behavior. Total strain energy density consisting of the plastic strain energy density and the elastic tensile strain energy density described fairly well the fatigue life of the steel, taking the mean stress effects into account. Compared to other fatigue damage parameters, fatigue life prediction by the cyclic strain energy density showed a good correlation with the experimental fatigue lift within a factor of 3.