• KSCE Journal of Civil and Environmental Engineering Research
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• v.12 no.1
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• pp.1-8
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• 1992

A method analizing contact pressure between plate and elastic half space is presented by using F.E.M. With the method, the pressure intensities at surface nodes of half space cae be directly calculated by using flexibility matrix of half space. The method is originally presented by Y.K. Cheung et al.(3) Insted of Y.K. Cheung's method, which use a conception of equi-contact pressure area around each surface nodes of half space in the noded rectanqular element area. We use the equi-contact pressure area around the Gaussian integration points of half space surface in the noded isoparametric element area. Numarical examples are presented and compared with other's studies.

• Transactions of the Korean Society of Mechanical Engineers
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• v.16 no.9
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• pp.1615-1626
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• 1992

In this study, vibrations and resulting acoustic radiations from an elastic beam impacted by a steel ball were studied theoretically and experimentally. First the transverse vibrations of free-free elastic beams are analysed with modal analysis technique. The impact forces are modeled with the Hertz's theory and the contanct duration is compared with the measured values. Also the calculated beam vibrations are verified with the experimental results. Then the acoustic radiations due to the beam vibration are studied numberically and experimentally. The acousticpressure is calculated assuming the beam has an elliptical cross-section. The predicted acoustic pressure is compared with the measured value. It was found that both the predicted beamvibrations using the Hertz's theory and the estimated acoustic pressure under the assumption of an elliptical cross- section are in very good agreements with the measured values.

• Tribology and Lubricants
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• v.28 no.6
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• pp.297-302
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• 2012

We conducted 3D elastic contact analysis of a sharkskin surface pattern for the characteristic assessment of biomimetic shark skin structure pattern for engineering applications. Rough sharkskin surfaces of similar size with real shark skin scales are generated numerically. Under the assumption of the contact of a plate on the generated sharkskin surface, contact performances such as contact pressure, real contact area, and surface separation are evaluated.

• Transactions of the Korean Society for Noise and Vibration Engineering
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• v.22 no.3
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• pp.253-263
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• 2012

With the local Hertz deformation on the contact point, the dynamic contact between a high-speed wheel and an elastic beam having a gap is numerically analyzed by solving the whole equations of motion of the wheel and the beam subjected to the contact condition. For the stability of the time integration the velocity and acceleration constraints as well as the displacement constraint are imposed on the contact point. Especially the acceleration contact condition on the gap is formulated, and it is demonstrated that the contact force variation computed by the velocity contact constraint or by the acceleration contact constraint agrees well with that computed by the displacement contact constraint. The numerical examples show that, when the wheel passes on the gap, the solution is governed by the stiffness of the local Hertzian deformation.

• Transactions of the Korean Society for Noise and Vibration Engineering
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• v.18 no.5
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• pp.541-549
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• 2008

The dynamic contact between a high-speed wheel and an elastic beam is numerically analyzed by solving the whole equations of motion of the wheel and the beam subjected to the contact condition. For the stability of the numerical solution, the velocity and acceleration constraints as well as the displacement constraint are imposed on the contact point. Through the numerical examples, it is shown that the acceleration contact constraint including the Coriolis and centripetal accelerations are crucial for the numerical stability.

• Proceedings of the KSME Conference
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• 2000.04a
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• pp.381-386
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• 2000

The brake force of drum brakes for commercial vehicles is applied by a s-cam. First of all the influence of the s-cam load angles and elastic modulus of the pad on the contact pressure distribution between pad and drum was checked by using 3 dimensional finite element model. In the second part, temperature and thermal stress analyses were carried out by an axisymmetric model with constant heat flux and pressure-proportional heat flux. In the case of temperature analysis the heat conduction from the interface to the pad and the drum was modeled using a thin soft film element, so artificial division of the generated heat flux between pad and drum is not necessary. The analysis was performed by ABAQUS/Standard code.

• Proceedings of the KSME Conference
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• 2001.06a
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• pp.889-894
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• 2001

A three dimensional transient thermo-elastic frictional contact analysis of airplane brakes is performed. The velocity history of the airplane during braking is calculated from energy conservation law. ABAQUS code is used in the analysis, and user subroutines supported in the ABAQUS are coded to calculate the frictional heat generation between pads and linings attached to back/pressure plate and rotor, respectively. Numerical results are compared with experimental ones.

• Transactions of the Korean Society of Automotive Engineers
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• v.9 no.3
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• pp.173-180
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• 2001

In the case of axisymmetric thermal analysis of drum brakes, the distribution of frictional heat produced on the interface and temperature difference between mating frictional faces are very interesting problems to computational researchers. In the first part, the influence of the s-cam load angles and elastic modulus of the pad on the contact pressure distribution between pad and drum was checked by a three dimensional model. In the second part heat conduction from the interface to the pad and the drum was modeled by using a thin interface element, so artificial division of the generated frictional heat between pad and drum is not necessary. Temperature difference between mating frictional faces is successfully modeled by using the interface element. The influence of some parameters on the thermal distribution is checked. The analysis was performed by ABAQUS/Standard code.

• Proceedings of the Korean Society for Technology of Plasticity Conference
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• 1998.06b
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• pp.19-27
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• 1998

박판금속성형공정을 통하여 컴퓨터를 이용한 계산방법으로 효율적이고 정확하게 해석할 수 있는 박판성형해석시스템인 SAIT_STAMP를 개발하였다. 또한 이를 현업문제에 적용하여 금형의 개발기간과 비용을 줄이고 성형품 품질저하 문제들을 해결하는데 이용하였다. SAIT_STAMP 는 성형해석, 성형후해석 프로그램과 전·후 처리기로 구성이 되어있다. 금형과 재료의 접촉 및 마찰을 고려한 새로운 접촉처리방법을 성형해석에 적용하여 해석속도와 해석정확도를 향상하였고 다단계성형 및 유압성형 등 박판성형에 필요한 대부분의 기능을 개발하여 적용하였다. 성형후해석은 성형해석의 결과를 토대로 스프링백해석을 수행한다. Visual C++을 사용하여 개발된 전·후 처리기는 window 95N/T 환경의 PC에서 수행된다. 개발된 프로그램을 이용하여 현업 문제에 적용 해석하였으며 상용S/W 대비 우수한 결과를 얻었다. 현재 삼성내 9개 관계사에서 설치되어 사용중이며 프로그램의 대외신뢰성확보를 위해 대학과 비경쟁업체에 프로그램을 설치하여 프로그램을 설치하여 프로그램의 시험과 성능향상을 하고 있다.

• Transactions of the Korean Society of Mechanical Engineers
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• v.2 no.3
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• pp.69-77
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• 1978

스폿 용접 기구를 탄성체로 생각하여 접촉 응력과 용접봉의 최적 형상을 구하였다. 접촉 응력은 2차 계획법 문제로 바꾸어 해석하였고, 이에 필요한 용접봉과 피용접판의 Flexibility matrix 들은 유한 요소법의 프로그램인 SAPIV 를 사용하였다. 최애 접촉 응력을 최소로 하는 용접봉의 형상설계를 위해 축차적인 선형 계획법을 적용하고 특정한 경우의 해를 도시하였다. 최적의 용접봉 모양은 중심부가 오목하고 가장자리 부분이 볼록한 형태로 나타났다.