• 한국해양공학회지
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• 제15권2호
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• pp.94-98
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• 2001

fatigue life and nondestructive evaluation were examined experimentally using surface crack specimen and compact tension specimen of 5083 aluminium alloy. Acoustic emission signals emanated during failure of aluminum alloys has been the subject of numerous investigations. Possible sources of AE during deformation have been suggested as the dislocations, fracture of brittle particles and debonding of these particles from the alloy matrix. Fatigue life and penetration behavior of long surface crack can be evaluated quantitatively using K values proposed by authors. The influence of stress ratio on the frequency characteristics of AE signals were investigated.

• 한국해양공학회지
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• 제13권2호통권32호
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• pp.58-65
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• 1999

The effect of specimen thickness on fatigue crack growth rate was studied. The objective of the present study is to investigate the effect of specimen thickness on the fatigue crack growth behavior at various stress intensity factor ranges and also the variation of material restance to fatigue crack growth. The fatigue crack growth resistance was treated as a spatial stochastic process, which varies randomly on the crack path, Compact tension specimens with a LT orientation for structural steel were used. All testing was done at a constant stress intensity level. The experimental data were analyzed for the size effect to determine the Weibull distributions of the material resistance.

• 한국공작기계학회:학술대회논문집
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• 한국공작기계학회 1996년도 춘계학술대회 논문집
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• pp.177-182
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• 1996

The objective of this thesis is to investigate the influence of welding residual stresses on the fatigue growth behavior of welding residual stresses on the fatigue growth behavior of cracks located transverse to the weld bead. For this purpose, G.T.A. (Gas Tungsten Arc) welding was performed on the Al. Alloy 1100-0 plate and the same initial crack is made on HAZ(Heat Affected Zone), weld metal and base metal respectively. C.T.(Compact Tension) specimens were used as experimental material. Initial welding residual stresses were measured by using strain gage sectioning method. All specimens were tested under constant amplitude load with stress ratio R=0.1

• Fibers and Polymers
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• 제5권4호
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• pp.259-263
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• 2004

Rubber-modified epoxy resins have been employed as adhesive and matrix materials for glass and corbon-fiber composites. The behavior of fracture around a crack tip for rubber-modified epoxy resin is investigated through the acoustic emission (AE) analysis of compact tension specimens. Damage zone and rubber particles distributed around a crack tip were observed by a polarized optical microscope and an atomic force microscope (AFM). The damage zone in front of pre-crack tip in rubber-modified specimen $(15wt\%\; rubber)$ began to form at about $13\%$ level of the fracture load and grew in size until $57\%$ load level. After that, the crack propagated in a stick-slip manner. Based on time-frequency analysis of AE signals and microscopic observation of damage zone, it was thought that AE signals with frequency bands of 0.15-0.20 MHz and 0.20­0.30 MHz were generated from cavitation in the damage zone and crack propagation, respectively.

• 한국해양공학회지
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• 제14권2호
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• pp.99-105
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• 2000

This paper describes the effect of specimen size on fatigue crack growth rate for the offshore structural high-tensile-strength steel BS4360 and machine structural steel SM45C. The purpose of the present study is to investigate the effect of stress ratio aspect ratio specimen width and specimen thickness of the fatigue crack growth behavior. Compact tension specimens with a LT orientation for BS4360 and SM45C steels were used, All testing was done at constant stress intensity factor range controlled fatigue crack growth condition. The investigation demonstrates that the fatigue crack growth rate is increased with increasing stress ratio and specimen thickness and is decreased with increasing specimen width. The fatigue crack growth rate is unaffected by aspect ratio until a/W=0.50 but is increased by increasing spect ratio from a/W=0.55.

• 한국안전학회지
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• 제12권2호
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• pp.57-64
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• 1997

Fatigue crack propagation behaviors and life prediction for SUS 321 plate and its electron beam weld metal were investigated using compact tension specimens. The larger the stress ratio is, the faster the crack propagates, but the variation of crack propagation rate decreases. The effect of stress ratio is greater in the slow crack propagation area than in the faster one. The crack propagation rate of electron beam weld metal is faster than that of base metal because of hardening, weld defect and residual stress in welding area. The crack propagation rate of transverse weld metal has a lower than that of base metal due to the effect of residual stress, but in the time of passing through welding area, has a higher rate. The crack propagation rate using $\Delta$K$_{eff}$ can be well plotted regardless of stress ratio. The fatigue life prediction method of considering crack closure more exactly predicts fatigue life than conventional one. conventional one.e.

• 한국광학회지
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• 제15권4호
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• pp.361-368
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• 2004

콤팩트디스크(CD-R; Compact DiskRecordable)를 성분별로 분리하여 제작하고, 다층 박막 구조를 만들어서 레이저빔의 에너지를 변화시켜 가면서 조사하여 각 성분 층에서의 최적 미소 점 마킹 조건과 홈 형성 과정에 관하여 연구하였다. 본 연구는 Q-스위치 Nd:YAG 레이저를 이용하여 준비된 각 시료의 표면에 27∼373 mJ 빔을 80 $\mu\textrm{m}$의 점적 크기로 조사하여 샘플에 형성된 흠 형태를 광학현미경(OM; Optical Microscope)과 광 결맞음 단층촬영기(OCT; Optical Coherence Tomography)로 비교-관찰하여 미소 점 마킹의 형성 과정을 분석하였다. 다층 박막에서 용융된 기판 층은 짧은 시간동안 충분한 열 흐름이 발생하여 증배의 형성을 야기하며, 반사 층과 염료 층 사이에 흡수된 에너지는 염료를 용융시키고 체적을 증가시켰으며, 증배가 식으면서 표면장력의 영향 및 레이저빔에 의한 순간적인 시편의 온도상승으로 기화와 반동압력에 의한 질량흐름 때문에 두 층의 경계면에서 홈과 외륜의 발생을 설명할 수 있었다. 따라서 다층 박막에서의 미소 점 마킹의 형성 과정은 표면장력, 용융 점성력, 층 두께, 다층 박막 성분 물질의 물리화학적ㆍ광학적 성질과 관계가 있음을 알 수 있었다.

• Journal of the Korean Wood Science and Technology
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• 제43권6호
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• pp.868-875
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• 2015

목구조물 접합부에 기존의 슬릿(slit)형 강판을 대체하기 위해서 FRP (Fiber Reinforced Plastic) 보강적층판을 제작하였다. 보강재, 접착제 종류에 따라 총 4가지 타입의 FRP 보강적층판을 제작하였으며, 접합부 적용 전 KSF 3021과 KSF 2160에 의거한 박리실험과 ASTM D5045-99에서 제안한 Compact Tension (CT)형 파괴인성 시험을 실시하였다. 접착성능 시험결과 GFRP textile, GFRP sheet, GFRP Textile-Sheet 타입의 FRP 보강적층판은 침지 및 내수침지박리 시험에서 모두 KS 기준인 박리율 5% 이하를 만족하였다. 그러나 Aramid 타입의 시험편은 침지박리율 4.8%로 기준을 만족하였으나 내수침지박리율 70%로 합격기준을 만족하지 못하였다. 파괴인성 시험결과 단판만을 교차적층 시킨 대조군시험편보다 목재 대비 보강재 체적비를 23%로 함으로서 FRP 보강적층판의 내력이 2~4배 증가하였다. 그중에서도 GFRP Textile-Sheet 타입의 시험편이 하중 평행방향의 유리섬유 배열로 인해 할렬파단을 억제하면서 대조군 대비 응력확대계수 비가 61% 증가되어 파괴를 가장 크게 억제하는 것으로 확인되었다. FRP 보강적층판과 비금속 dowels을 사용한 접합부의 인장형 전단내력은 금속접합에 비해 약 12% 낮은 내력이 측정되었다.

• 대한토목학회논문집
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• 제5권3호
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• pp.161-175
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• 1985

판항교(鈑桁橋)의 덮개 판(板), 수직보강재(垂直補强材) 및 연결판(連結板) 등의 용접연결부(鎔接連結部)를 포함하는 실물(實物)을 modeling 하여 직접(直接) 피로시험(疲勞試驗)을 행하지 않고서도 계산 program에 의해 S-N 선도(線圖)를 그리는 방안을 정립하여 서울의 수동대교(水東大橋), 제(第) 3 한강교(漢江橋) 및 춘천(春川)의 강촌교(江村橋) 등에 적용해 보았다. 이에 앞서, SS 41, SS 50, SWS 50, SWS 58 등의 구조강(構造鋼)으로서 소재(素材), 균열방향에 평행용정, 균열방향에 직각 용접의 compact tension 시험편을 제작 피로시험을 행하여 계산 program 중의 data로 쓰여질 재료상수(材料常數) c 및 m 값을 구하였다. 이 결과 다음과 같은 결과들을 얻었다. 덮개판(板)의 경우 다른 두 부분보다 피로강도(疲勞强度)가 매우 낮았다. 덮개판(板)의 경우 두께가 커지면 피로강도(疲勞强度)가 상당히 낮아지는 외에는 치수에 그다지 큰 영향을 받지 않으며, c 및 m 값에는 매우 민감한 영향을 받음을 알 수 있었다. c 값 및 m 값이 적어질수록 피로강도(疲勞强度)가 상당히 커지며, m 값이 적어지면 S-N 곡신의 경사가 매우 급해짐을 알 수 있었다. 이와 같은 연구가 계속되어 더 많은 data가 집적(集積)되면 앞으로 설계(設計)될 판항교(鈑桁橋)의 피로설계지침(疲勞設計指針)을 마련하고, 또 기존(旣存) 판항교(鈑桁橋)의 피로(疲勞)에 대한 내용년한(耐用年限)을 추정(推定)할 수 있는 기본(基本) pattern이 제공(提供)할 수 있으리라 사료된다.

• 대한기계학회논문집
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• 제18권9호
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• pp.2331-2338
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• 1994

Experimental conditions of the optical shadow methods of caustics for measurement of the stress intensity factor and the J-integral in various materials(polycarbonate, PMMA, Al 5586D) are investigated. The necessary experimental requirements toe determine accurate values of the stress intensity factors and the J-integrals are described. The ratio of $r_o$ (radius of initial curve) to $r_p$ (plastic zone size) is selected as a parameter to verify the experimental limitation of the method of caustics in determination of fracture parameters. In this study, transmission caustics method was used for compact tension specimens made of polycarbonate and PMMA. while reflection caustics method was applied to c-shaped tension specimen made of Al 5586D. The appropriate ranges of $r_o/r_p$ tp determine accurate values of stress intensity factors were found to be 1.5~1.8. Existing experimental results have been obtained mainly by changing $r_p$ with different loads in $r_o/r_p$. However, in this study we could obtain varying $K_{caus}/K_{th}$ over the wide range of $r_o/r_p$ at fixed load conditions with newly designed optical arrangement. Thus, we could find the range in which theoretical and experimental results agree well each other by changing $r_o$ values only. In Al 5586D specimen, experimental caustics were located inside of the plastic zone, and $K_{caus}/K_{th}$ were found to be not unity in this range. It is found that $J_{caus}/J_{th}=1{\;}with{\;}r_o/t{\geq}0.8$ and the experimental plastic zone includes the contours of caustics.