• 한국해양공학회지
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• 제18권1호
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• pp.28-34
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• 2004

It is well known that tensile peak overloads may significantly delay suubsequent constant amplitude fatigue crack growth in many materials. Since real structures are usually subjected to complex load histories, the ability to predict accurate crack growth under realistic service conditions is of major engineering interest. This paper describes experiments on fatigue track growth in the integrally stiffened panel of 7075-T6 aluminum alloy. The effect of shape parameters and overload position on the fatigue crack growth behavior of integrally stiffened panels are discussed. Based on the experimental results, the following conclusions have been drawn: the overall fatigue crack growth retardation resulting from single overload in the stiffened panels was generally larger in the larger thickness ratio, although the retardation trends, according to the change in overload positions, were similar to those exhibited in the non-stiffened panels.

• 콘크리트학회논문집
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• 제21권4호
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• pp.481-488
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• 2009

시멘트페이스트, 모르타르 및 콘크리트의 자기수축의 크기 및 발현율은 초기재령 내부온도의 이력과 크기에 의해 영향을 받는다고 보고된 바 있으나, 초기재령 수화열과 자기수축에 대한 구체적인 관계분석은 아직 미흡한 실정 이다. 이 연구에서는 초기재령 수화온도 및 자기수축의 이력특성에 대한 분석방법을 제시한 선행연구를 기초로, 시험체 크기 및 수화지연 효과에 따른 고강도콘크리트의 초기재령 수화열과 자기수축의 거동특성 및 상관관계를 분석하였다. 또한 자기수축에 의한 균열평가시 유효자기수축의 기준이 되는 응결시간과 수화온도 및 자기수축의 이력과의 관계도 검토하였다. 그 결과, 시험체가 매스화될수록 초기재령 수화발열 상승구간의 수화온도 상승량 및 수화발열 상승속도, 자 기수축 증가구간의 자기수축 증가량 및 자기수축 속도는 증가하는 것으로 나타났으며, 지연제를 사용할 경우 그 값은 감소하는 것으로 나타났다. 초기재령 콘크리트의 수화발열 상승속도가 증가하면 자기수축 속도는 증가하며, 이와 더불 어 재령 91일 자기수축도 증가하는 것으로 나타나, 종국 자기수축은 초기재령 수화발열상승 속도에 의해 영향을 받을 수 있을 것으로 사료된다. 한편, 콘크리트 균열평가시 유효자기수축의 기준이 되는 응결시간과 변곡점 및 수화온도 상 승시점은 시멘트의 수화반응 과정에 있어 서로 밀접한 관계가 있음을 확인할 수 있었다.

• 한국생산제조학회지
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• 제6권4호
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• pp.80-88
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• 1997

An experimental investigation of the fatigue through crack growth behavior under simple stepped variable loading condition has been performed using Al7075-T651. Experiments were carried out by using cantilever bending type specimens, with chevron notches on a small electro-magnetic test machine. Tensile overloads have a retarding effect on the fatigue crack growth rates, therefore tensile overloads were used for the beneficial effect on the fatigue life. While in most cases compressive overloads have only a vanishing effect on crack growth rates, some experiments with single edge crack tension specimens reveal a marked growth retardation. The stress ratios used in this investigations varies from R=0.32 to 0.81, from R=0.04 to 0.76, from R=-0.15 to 0.73, and from R=-0.33 to 0.68 and the peak load for each case was not varied. The crack growth and crack closure were measured by Kikukawa's compliance method with a strain gauge mounted on the backside of each specimens. The results obtained are as follows. When the stepped variable load was applied, the smaller the stress ration was, the larger the delayed retardation of the crack growth rate was. The fatigue crack growh rate data obtained for through cracks were plotted well against the effective stress intensity factor range from 4.0 to 20.0MP{a^{SQRT}m}. It was found that the effective stress intensity factor range ratio was related well to the opening stress intensity factor, the maximum stress intensity factor, and crack length.

• 대한기계학회논문집A
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• 제26권8호
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• pp.1487-1494
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• 2002

In this study, to propose the prediction method of the crack growth under flight-simulation loading, crack growth tests are conducted on 2124-7851 aluminum alloy specimens. The prediction of crack growth under flight-simulation loading is performed by the stochastic crack growth model which was developed in previous study. First of all, to reduce the complex load history into a number of constant amplitude events, rainflow counting is applied to the flight-simulation loading wave. The crack growth, then, is predicted by the stochastic crack growth model that can describe the load interaction effect as well as the variability in crack growth process. The material constants required in this model are obtained from crack growth tests under constant amplitude loading and single tensile overload. The curves predicted by the proposed model well describe the crack growth behavior under flight-simulation loading and agree with experimental data. In addition, this model well predicts the variability of fatigue lives.

• 한국광학회지
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• 제14권1호
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• pp.44-50
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• 2003

반도체 레이저 측면 여기시 Nd:YAG 레이저 매질에서 발생하는 열영향에 대해 분석하였다. 열영향을 고감도로 측정하기 위해 편광자와 Nd:YAG 매질 사이에 λ/4판을 삽입하여 여기 파워에 따라 발생하는 depolarization양을 측정하였다. CCD로 는 열영향에 의한 매질 내에서의 탐침광 분포 변화를 측정하고 해석하여 반도체 레이저 측면 여기시 발생하는 열영향을 최소화하기 위한 공진기 설계의 효과적인 방법을 제시하였다.

• 한국정보디스플레이학회:학술대회논문집
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• 한국정보디스플레이학회 2009년도 9th International Meeting on Information Display
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• pp.597-599
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• 2009

We have developed new type of LCD Device which enables switching from reflective to tranmissive LCD mode and vice versa according to brightness of the surrounding. Alternation in these modes are possible by adding on circular polarized sheet and retardation film onto the bottom polarizer which allows the control of the back light and the LCD cell gamma voltage depending on the atmosphere. This method has been evaluated and confirmed by running on the LCD module device in which we have optimized retardation value by Poincare polarizer analysis.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 1994년도 추계학술대회 논문집
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• pp.826-830
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• 1994

Making Brinell indentations facing each other near the crack tip is very effective method in increasing fatigue life. In this paper, fatigue test was performed after indentation to investigate the effect of thickness of specimen. The results show that fatigue lives increased my making indentation and retardation cycle is inverse proportional to thickness of specimen.

• 한국생물물리학회:학술대회논문집
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• 한국생물물리학회 1997년도 학술발표회
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• pp.21-21
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• 1997

Transport of drug entrapped in a liposome-hydrogel formulation was significantly retarded in an in vitro topical application. Liposomes containing hydrocortisone acetate, a hydrophobic antiinflammatory agent, were prepared by the precipitation method, and the liposomal suspension was mixed with hydrogel into a semisolid gel-type ointment.(omitted)

• 한국조명전기설비학회지:조명전기설비
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• 제5권2호
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• pp.84-95
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• 1991

Mostly, phase control method is used to control the single phase AC power. The phase control method has some advantages such as ease to control and simple configuration. But the retardation of firing angle causes a lagging current even if load is purely resistive. So phase control causes a lagging power factor and a low efficiency at the input side in comparing with the system without switching device. A new PWM control method which can improve these defects for single phase AC power control circuit is proposed in this paper. The performances of the single phase AC power control circuit using the proposed method was investigated theoretically. Both power factor and waveform of load current can be improved better than those of the conventional methods.

• 대한기계학회논문집A
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• 제35권11호
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• pp.1415-1422
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• 2011

운송기계구조물의 제작에 사용되는 판재 알루미늄 합금재료는 일정한 피로응력조건하에서 두께에 따라 균열진전속도의 차이를 보인다. 이러한 두께효과는 판재 알루미늄합금의 주요한 피로파괴특성 중 하나이다. 본 연구에서는 일정한 피로응력조건하에서 실시한 후판 및 박판 Al 2024-T3 합금재료의 피로 시험을 통하여 두께효과를 파악하고, 이를 형상인자인 두께비, $R_t$ 및 하중인자인 두께별 등가유효응력확대비, $U_{i}^{equ}$에 의한 상호관계식, $U_{i}^{equ}=f(R_t)$로 나타내었다. 그리고 두께효과에 의한 후판 대비 박판시험편의 균열진전 지연거동을 ${\Delta}K$ 환산법을 사용하여 정량적으로 분석하였다. 두께효과의 경향을 정량으로 나타내기 위해 두께감소율(DoT)과 응력확대계수범위, ${\Delta}K$의 감소율(DoS) 등의 값을 구하여 이들 상호관계를 규명하였다.