• 한국소성가공학회:학술대회논문집
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• 한국소성가공학회 2008년도 추계학술대회 논문집
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• pp.333-336
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• 2008

The groove rolling is a process that transforms the bloom or billet into a shape with circular section through a series of rolling. Inhibition of surface defect generation in groove rolling is a matter of great importance and therefore many research groups proposed a lot of models to find the location of surface defect initiation. In this study, we propose a model for maximum shear stress ratio over equivalent strain to catch the location of surface defect onset. This model is coupled with element removing method and applied to box groove rolling of POSCO No. 3 Rod Mill. Results show that proposed model in this study can find the location of surface defect initiation during groove rolling when finite element analysis results is compared with experiments. The proposed criterion has been applied successfully to design roll grooves which inhibits the generation of surface defect.

• 소성∙가공
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• 제17권8호
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• pp.607-612
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• 2008

The groove rolling is a process that transforms the bloom or billet into a shape with circular section through a series of rolling. Inhibition of surface defect generation in groove rolling is a matter of great importance and therefore many research groups proposed a lot of models to find the location of surface defect initiation. In this study, we propose a model for maximum shear stress ratio over equivalent strain to catch the location of surface defect onset. This model is coupled with element removing method and applied to box groove rolling of POSCO No.3 Rod Mill. Results show that proposed model in this study can find the location of surface defect initiation during groove rolling when finite element analysis results is compared with experiments. The proposed criterion has been applied successfully to design roll grooves which inhibit the generation of surface defect.

• 한국융합학회논문지
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• 제9권5호
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• pp.151-156
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• 2018

본 연구에서는 CFRP와 금속 또는 비금속을 접착제로 접합시켜 이 재료에 대한 파손 연구를 수행하였다. 그 해석 조건으로는 DCB 시험편을 이용하여 시험편의 상부에는 CFRP, 시험편의 하부에는 금속 또는 비금속 재료로 지정하였고 두 상부와 하부 사이를 구조용 접착제로 부착하는 것을 묘사하였다. 이 해석 결과로는 알루미늄으로 접착된 시험편에서 가장 작은 등가응력 보였고 티타늄을 사용하였을 때 박리된 CFRP시험편에서의 최대 전단응력은 가장 낮음을 보였다. 결론적으로 티타늄을 사용하였을 때 시험편의 변형이 가장 작은 것을 알 수 있었고 본 연구 결과를 토대로 접착제를 이용한 접착 계면의 파손데이터를 실생활에 융합하여 그 미적 감각을 나타낼 수 있다.

• 예술인문사회 융합 멀티미디어 논문지
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• 제8권3호
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• pp.589-596
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• 2018

현대 사회에서 의식주 중에서 구조물이나 운송수단은 중요한 역할을 가진다. 만약 구조물이나 운송수단에 작은 크랙이라도 생기고 크랙이 진전되면 그 부품들이 파괴되어 큰 사고를 야기할 수 있다. 이러한 상황을 방지하기 위한 본 연구에서는 크랙의 진전에 따른 파손 경향을 조사하기 위하여 시험편을 이용하였다. CT 시험편의 재질로는 요즘 각광받는 복합재료인 단방향 탄소섬유 강화플라스틱을 사용하였다. 시험편 모델은 단방향성 섬유로서 적층각도를 주었고 적층각도는 [60/-60/60/-60]순으로 지정하였다. 해석 조건으로는 하단부의 홀을 고정시킨후 상단부 홀을 15mm의 강제 변위를 가하였다. 본 연구 결과로는 구조용 강, 구리, 티타늄, 알루미늄 순으로 등가응력과 전단응력이 높게 나왔다. 이러한 결과는 이종재료로 만들어진 CT 시험편의 파손을 검증하는 데 유용하게 사용될 수 있다고 사료된다.

• 한국지진공학회논문집
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• 제12권3호
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• pp.11-20
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• 2008

본 연구에서는 저경도 고감쇠 고무받침 시험체의 다양한 특성실험을 통하여 저경도 고감쇠 고무받침의 특성을 파악하였다. 고무받침의 파악하고자 하는 특성은 압축강성, 전단강성, 등가감쇠비, 전단특성의 변형율 의존성, 전단특성의 면압 의존성, 전단특성의 주파수 의존성, 전단특성의 온도 의존성, 극한전단특성 등이다. 특성실험은 ISO 22762-1에 따라 수행하였으며, ISO 2276-3에 따라 평가하였다. 특성실험결과 전단강성은 전단변형율과 온도 의존성이 큰 것으로 나타났고, 등가감쇠비는 면압 의존성이 큰 것으로 나타났다. 전단특성의 주파수 의존성 실험결과 0.1Hz를 기준으로 경향이 나뉘는 것으로 나타났다. 0.1Hz 이상에서는 전단특성의 변화가 적었지만, 0.1Hz 이하에서는 전단강성과 등가감쇠비 모두 급격히 감소하는 것으로 나타났다. 추가적으로 크리프실험과 극한전단특성실험을 수행하였고, 실험결과는 ISO 22762-3의 요구사항을 만족하는 것으로 나타났다.

• Journal of Pharmaceutical Investigation
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• 제39권3호
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• pp.185-199
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• 2009

Using a strain-controlled rheometer [Advanced Rheometric Expansion System (ARES)], the steady shear flow properties and the dynamic viscoelastic properties of $Antiphlamine-S^{(R)}$ lotion have been measured at $20^{\circ}C$ (storage temperature) and $37^{\circ}C$ (body temperature). In this article, the temperature dependence of the linear viscoelastic behavior was firstly reported from the experimental data obtained from a temperature-sweep test. The steady shear flow behavior was secondly reported and then the effect of shear rate on this behavior was discussed in detail. In addition, several inelastic-viscoplastic flow models including a yield stress parameter were employed to make a quantitative evaluation of the steady shear flow behavior, and then the applicability of these models was examined by calculating the various material parameters. The angular frequency dependence of the linear viscoelastic behavior was nextly explained and quantitatively predicted using a fractional derivative model. Finally, the strain amplitude dependence of the dynamic viscoelastic behavior was discussed in full to elucidate a nonlinear rheological behavior in large amplitude oscillatory shear flow fields. Main findings obtained from this study can be summarized as follows : (1) The linear viscoelastic behavior is almostly independent of temperature over a temperature range of $15{\sim}40^{circ}C$. (2) The steady shear viscosity is sharply decreased as an increase in shear rate, demonstrating a pronounced Non-Newtonian shear-thinning flow behavior. (3) The shear stress tends to approach a limiting constant value as a decrease in shear rate, exhibiting an existence of a yield stress. (4) The Herschel-Bulkley, Mizrahi-Berk and Heinz-Casson models are all applicable and have an equivalent validity to quantitatively describe the steady shear flow behavior of $Antiphlamine-S^{(R)}$ lotion whereas both the Bingham and Casson models do not give a good applicability. (5) In small amplitude oscillatory shear flow fields, the storage modulus is always greater than the loss modulus over an entire range of angular frequencies tested and both moduli show a slight dependence on angular frequency. This means that the linear viscoelastic behavior of $Antiphlamine-S^{(R)}$ lotion is dominated by an elastic nature rather than a viscous feature and that a gel-like structure is present in this system. (6) In large amplitude oscillatory shear flow fields, the storage modulus shows a nonlinear strain-thinning behavior at strain amplitude range larger than 10 % while the loss modulus exhibits a weak strain-overshoot behavior up to a strain amplitude of 50 % beyond which followed by a decrease in loss modulus with an increase in strain amplitude. (7) At sufficiently large strain amplitude range (${\gamma}_0$>100 %), the loss modulus is found to be greater than the storage modulus, indicating that a viscous property becomes superior to an elastic character in large shear deformations.

• Structural Engineering and Mechanics
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• 제75권5호
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• pp.559-569
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• 2020

In the present study, the fracture toughness of U-shaped notches made of aluminum alloy Al7075-T6 under combined tension/out-of-plane shear loading conditions (mixed mode I/III) is studied by theoretical and experimental methods. In the experimental part, U-notched test samples are loaded using a previously developed fixture under mixed mode I/III loading and their load-carrying capacity (LCC) is measured. Then, due to the presence of considerable plasticity in the notch vicinity at crack initiation instance, using the Equivalent Material Concept (EMC) and with the help of the point stress (PS) and mean stress (MS) brittle failure criteria, the LCC of the tested samples is predicted theoretically. The EMC equates a ductile material with a virtual brittle material in order to avoid performing elastic-plastic analysis. Because of the very good match between the EMC-PS and EMC-MS combined criteria with the experimental results, the use of the combination of the criteria with EMC is recommended for designing U-notched aluminum plates in engineering structures. Meanwhile, because of nearly the same accuracy of the two criteria and the simplicity of the PS criterion relations, the use of EMC-PS failure model in design of notched Al7075-T6 components is superior to the EMC-MS criterion.

• 한국정밀공학회지
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• 제12권11호
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• pp.98-109
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• 1995

An investigation was performed to study the inner damage of laminated composite plates subjected to out-of-plane load. During the investigation, inpact velocity and equivalent static load relationship was derived. Reddy's higher-order shear deformation theory(HSDT) and Hashin's failure criteria were used to determine inner stresses and damaged area. And impact testing was carried out on laminated composite plates by air gun type impact testing machine. The CFRP specimens were composed of [ .+-. 45 .deg. ]$_{4}$and [ .+-. 45 .deg. /0 .deg. /90 .deg. ]$_{2}$ stacking sequences with 0.75$^{t}$ * 26$^{w}$ * 100$^{l}$ (mm) dimension. After impact testing. As a result, a relationship holds between damaged area and impact energy, and a matrix cracking was caused by the interlaminar shear stress in the middle ply and was caused by the inplane transverse stress in the bottom ply.

• Structural Engineering and Mechanics
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• 제68권2호
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• pp.183-191
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• 2018

In this paper, harmonic responses of infilled multi-storey frames are obtained by using a single variable shear deformation theory (SVSDT) and dynamic stiffness formulations. Two different planar frame models are used which are fully infilled and soft storey. The infill walls are modeled by using equivalent diagonal strut approach. Firstly, free vibration analyses of bare frame and infilled frames are performed. The calculated natural frequencies are tabulated with finite element solution results. Then, harmonic response curves (HRCs) of frame models are plotted for different infill wall thickness values. All of the results are presented comparatively with Timoshenko beam theory results to reveal the effectiveness of SVSDT which considers the parabolic shear stress distribution along the frame member cross-sections.

• 한국소성가공학회:학술대회논문집
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• 한국소성가공학회 2001년도 춘계학술대회 논문집
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• pp.205-208
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• 2001

Localized shear band is investigated through the analysis of one-dimensional model for simple shearing deformation of thermally rate dependent material. Generally mesh size or interval of nodes play an important role in determining the overall flow behavior of the material. In order to observe these size effects we adapted non-local theory by including higher order strain gradients of the equivalent strain into the constitutive equation for the flow stress. for the ease of convergence and numerical stability the inplicit finite difference scheme is employed.