• 콘크리트학회지
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• 제7권4호
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• pp.149-156
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• 1995

경량기포콘크리트(ALC : Autoclaved Lightweight Concrete)의 내구성을 개선하기 위하여 투숩 및 투수, 편면동결융해 특성과 탄산화 특성을 실험하였다. 국산 ALC전용마감재는 방수용 도장재에 가까운 투습 및 투수성질을 갖고 있어 특성의 개선이 요구된다. 편면동결융해시험에서 마감재의 투습도에 따른 열화위치는 투습도가 클수록 외측에서 발생하였으나 투수에 의한 외부의 박리열화는 관찰되자 않았다. 탄산화는 수분의 함량이 작을수록 빠르게 진행되었으며 탄산화가 진행됨에 따라 기공량은 감소하였다. 탄산화가 완전히 진행되면 부피의 팽창으로 균열이 발생하였다.

• 콘크리트학회지
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• 제6권3호
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• pp.201-214
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• 1994

본 연구는 콘크리트용 혼화재로서 우리나라에 풍부한 천연 실리카 질 광물을 이용하여 콘크리트의 강도증진 가능성 및 유용성과 경제적인 효율성에 대해 검토한 것이다. 제반 실험을 통해 얻어진 결론을 요약하면 다음과 같다. \circled1 최적의 제오라이트 치환율은 단위 시멘트당 5~10% 정도를 나타났으며, 그 때의 강도 증진율은 무첨가 콘크리트 값에 비해 대체적으로 40%정도의 강도증진 효과를 얻었다. \circled2 최적의 이암 치환율은 단위 시멘트량당 10~15% 정도로 나타났으며, 그때의 강도 증진율은 무첨가 콘크리트 값에 비해 대체적으로 10%정도의 강도증진 효과를 얻었다. 이러한 검토로부터 우리는 혼화재로서 콘크리트의 강도성능의 향상을 목적으로 기존의 실리카 흄, 플라이 애쉬 등의 대체품으로 천연 실리카 광물을 활용할 수 있다는 결론을 얻었다.

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 1995년도 봄 학술발표회 논문집
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• pp.35-41
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• 1995

Fracture Mechanics does work for concrete, provided that a finite nonlinear zone at fracture front is being considered. The development of model for fracture process zone is most important to describe fracture phenomena in concrete. The fracture process zone is a region ahead of a traction-free crack, in which two major mechanisms, microcracking and bridging, play important rules. The toughness due to bridging is dominant compared to toughness induced by microcracking, so that the bridging is dominant mechanism governing the fracture process of concrete. In this paper the bridging zone, which is a part of extended macrocrack with stresses transmitted by aggregates in concrete, is model led by a Dugdale-Barenblatt type model with linear tension-softening curve. Two finite element techniques are shown for the model of fracture process zone in concrete.

• 대한기계학회논문집A
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• 제27권2호
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• pp.317-326
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• 2003

The influence of cyclic bending moment on the delamination and the fatigue crack propagation behavior in Al/GFRP laminate such as the wing section was investigated. The main objective of this study was to evaluate the relationship between crack profile and delamination behavior. And a propose parameter on the delamination growth rate(d $A_{D}$/da) of Al/GFRP laminates with a saw-cut using relationship between delamination area( $A_{D}$) and cycles(N), crack length(a), stress intensity factor range($\Delta$K). Also, the fiber bridging effect factor( $F_{BE}$ ) was propose that the fiber bridging modification factor($\beta$$_{fb}$ ) to evaluate using the delamination growth rate(d $A_{D}$/da). The shape and size of the delamination zone formed along the fatigue crack between aluminum alloy sheet. Class fiber-adhesive layer were measured by an ultrasonic C-scan image. The shape of delamination zone turns out to be semi-elliptic with the contour decreased non-linearly toward the crack tip. It represents that relationship between crack length and delamination growth rate(d $A_{D}$/da) were interdependent by reciprocal action, therefore it's applicable present a model for the delamination growth rate(dA/sib D//da) in Al/GFRP laminates.minates.s.

• 한국콘크리트학회:학술대회논문집
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• 한국콘크리트학회 1993년도 봄 학술발표회 논문집
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• pp.65-72
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• 1993

Steel fiber reinforced concrete(SFRC) which is made by short, randomly distributed steel fibers in concrete is superior in its tensile mechanical properties to plain concrete in enhancement of tensile strength and tensile ductility. These improvements are attributed to crack arresting mechanism and formation of longer crack paths due to fibers , which as a consequence lead to increase in energy absorption capacity of SFRC. In the post-peak region under tensile stresses, major macrocrack forms at critical section. The opening of this macrocrack is mainly resisted by both of the fiber pull-out bridging the cracked surfaces and the resistance by matrix softening. In this study, micromechaincal approach has been made in order to simulate tensile behavior of SFRC and based on which the theoretical model is presented. This model reflects the features of both the composite material concept and the spacing concept in predicting tensile strength of SFRC. The model also takes into account for the effects of matrix tensile softening and fiber bridging by pull-out on the resistance for the post-peak behavior of SFRC. It has been shown that the developed model satisfactory predicts the experimental results.

• Structural Engineering and Mechanics
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• 제30권2호
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• pp.147-164
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• 2008

Recently, many researches have been done to examine the behavior of fiber reinforced concrete (FRC) subjected to the static loading. However, a few studies have been devoted to cyclic behaviors of FRC. A main objective of this paper is to investigate the cyclic behavior of FRC through theoretical method. A new cyclic bridging model was proposed for the analysis of fiber reinforced cementitious composites under cyclic loading. In the model, non-uniform degradation of interfacial bonding under cyclic tension was considered. Fatigue test results for FRC were numerically simulated using proposed models and the proposed model is achieving better agreement than the previous model. Consequently, the model can establish a basis for analyzing cyclic behavior of fiber reinforced composites.

• 한국콘크리트학회:학술대회논문집
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• 한국콘크리트학회 2006년도 춘계 학술발표회 논문집(II)
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• pp.365-368
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• 2006

In this paper, the post cracking stress-crack width relationship of the composite is studied from a micromechanics points of view. Cook-Gordon debonding effect is studied by more refined method with considering of chemical friction of fiber interface. As a result, fiber with pre-debonding length retards stress development and shows more wide crack width for the same force level. longer pre-debonding length and lower pre-debonding bond strength results in lower full-debonding force, but same crack width.

• 콘크리트학회논문집
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• 제21권5호
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• pp.541-548
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• 2009

지금까지 ECC의 인장거동 예측에 대한 이론적인 연구는 균열면에서 섬유가 균일하게 분산되어 있다고 가정하고 섬유 가교 곡선을 유도하는 방법으로 수행되었으며, 섬유의 기울어진 각도와 섬유사이의 간격은 섬유 가교 곡선을 예측하는데 큰 영향을 준다. 그러나 이론적으로 유도된 방법은 섬유의 기울어진 각도와 섬유 간격에 따라서 섬유가교 곡선의 형태가 달라지는 것을 모사하지 못하여 실제 섬유 가교 곡선과 차이를 보이며, ECC 인장거동을 예측할 때 큰 오차가 발생할 수 있다. 이 연구에서는 이러한 문제점을 해결하기 위하여 균열면에서 섬유 가교 작용에 기여하는 유효 섬유의 개수를 섬유의 기울어진 각도와 섬유 간격에 따라 고려한 후, 수정된 섬유 가교 곡선을 구하고, 이를 이용하여 보다 합리적인 ECC의 인장거동 예측기법을 제시하였다. 또한, 인장거동 예측에 중요한 변수인 초기 균열 강도, 섬유 가교 곡선에서의 최고 응력과 변위, 인장변형률, 균열간격을 구하기 위한 방법과 절차를 제시하였다. 그리고 예측 방법의 타당성을 평가하기 위하여 수정된 섬유 가교 곡선과 이론적인 섬유 가교 곡선으로 구한 ECC의 인장거동을 실험 결과와 비교하였다. 수정된 섬유 가교 곡선을 사용할 경우, 실험 결과와 잘 일치함을 알 수 있었으며, ECC의 인장거동을 합리적으로 예측할 수 있을 것으로 판단된다.

• 대한기계학회논문집A
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• 제28권2호
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• pp.174-180
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• 2004

If Fiber Reinforced Metal Laminates(FRMLs) were delaminated, the decrease of stiffness and fiber bridging effect would result in the sudden aggravation of fatigue characteristics. It was reported that the delamination of FRMLs resulted from the crack of metal layers and that it depended on the crack growth. While cracks were made in FRMLs containing a saw-cuts under fatigue loading, cracks could be produced or not in FRMLs with circular holes under the same condition. When the FRMLs with the circular holes produce not the crack but the delamination, it is not possible to analyze it by the conventional fracture parameters expressed as the function of the crack. And so, this research suggests a new analytical model of the delamination to make the comparison of the delamination behavior possible whenever the cracks occur or not. Therefore, a new analytical model called Pseudo Crack Model(PCM) was suggested to compare the delaminations whether cracks were made or not. The relationship between the crack energy consumption rate( $E_{crack}$) and the delamination energy consumption rate( $E_{del}$) was discussed and it was also known that the effect of $E_{del}$ was larger than that of $E_{crack}$.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 춘계학술대회논문집A
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• pp.165-169
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• 2000

A simple method was suggested to calculate the stress intensity factor for a one-sided patched crack with finite thickness. To consider out-of-plane bending effect resulting from the load-path eccentricity, the spring constant as a function of the through-thickness coordinate z was calculated from the stress distribution in the un-cracked plate, ${\sigma}_{yy}(y=0,\;z)$, and the displacement for the representative single strip Joint, $u_y(y=0,\;z)$. The stress Intensity factors were obtained using Rose's asymptotic solution approach and compared with the finite element results. In short crack region, two results had a little difference. However, two results were almost same in long crack region. On the other hand, the stress intensity factor using plane stress assumption was more similar to finite element result than plane strain condition.