• Bulletin of the Society of Naval Architects of Korea
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• v.29 no.1
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• pp.21-32
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• 1992

• Journal of the Computational Structural Engineering Institute of Korea
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• v.21 no.1
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• pp.51-58
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• 2008

A constitutive model based on a combination of a micromechanics-based weakened interface elastic model (Lee and Pyo, 2007) and a crack nucleation model (Karihaloo and Fu, 1989) is proposed to predict the effective elastic behavior of particle-reinforced composites. The model specifically considers imperfect interfaces in particles and microcracks in the matrix. To exercise the proposed constitutive model and to investigate the influence of model parameters on the behavior of the composites, numerical simulations on uniaxial tension tests were conducted. Furthermore, the present prediction is compared with available experimental data in the literature to verify the accuracy of the proposed constitutive model.

• Journal of Korean Orthopaedic Sports Medicine
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• v.2 no.2
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• pp.113-118
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• 2003

Throwing motion divided by 6 phases such as wind-up, (early and late) cocking, acceleration, deceleration, follow-through. Overuse injuries in baseball result most often from pitching. Poor mechanics is the leading cause of arm injuries. The purpose of this article is to analyze the each joint motion and evaluate the biomechanics and pathomechanics during pitching.

• Proceedings of the Computational Structural Engineering Institute Conference
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• 2009.04a
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• pp.18-20
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• 2009

입자 강화 복합재료 내에서의 다양한 손상 메커니즘은 복합재료의 전체 거동을 예측에 상당한 영향을 미친다. 이에 본 연구에서는 입자 강화 복합재료 내에서의 누적 손상을 고려한 미세역학 기반 탄소성 모델(Kim and Lee, 2009)을 소개하고자 한다. Kim and Lee (2009)에 의해서 입자 강화 복합재료의 탄소성 모델을 위해 입자 강화 복합재료 내 계면에서의 누적 손상 및 기지재의 연성 거동이 고려되었다. 제안된 모델을 이용한 입자 강화 복합재료의 탄소성 거동 예측값은 관련된 실험값 (Llorca et al., 1991)과의 비교를 통해 수치해석을 수행하였다.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.30 no.2 s.245
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• pp.112-119
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• 2006

Due to their intrinsic anisotropy, composite materials show quite complicated damage mechanism with their fiber orientation and stacking sequence and especially, their fatigue damage process is sequential occurrence of matrix cracking, delamination and fiber breakage. In the study, to propose new model capable of describing damage mechanism under fatigue loading, fatigue analysis of composite laminates based on damage mechanics, are performed. The average stress is disassembled with stress components of matrix, fiber and interlaminar interface through stress analysis. Each stress components are used to assess static damage analysis based on continuum damage mechanics (C.D.M.). Fatigue damage curves are obtained from hysteresis loop and assessed by the fatigue damage analysis. Then, static and fatigue damage analysis are combined. Expected results such as stress-cycle relation are verified by the experimental results of fatigue tests.

• Proceedings of the Computational Structural Engineering Institute Conference
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• 2011.04a
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• pp.123-126
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• 2011

본 논문에서는 점탄성 매트릭스와 탄성 강화입자로 구성된 복합재료의 크리프 거동예측을 미세역학 기반의 시뮬레이션을 통하여 수행하였다. 에폭시 고분자로 이루어진 복합재료의 경우 재료 특성상 탄성적 거동뿐 아니라 점성적 거동도 함께 발생하게 된다. 이렇듯 점탄성 거동을 보이는 재료의 경우 탄성만을 고려한 해석방법으로는 한계가 있으며 점성적인 특성 또한 고려되어야 한다. 점탄성 복합재료의 해석을 위해서 손상을 고려한 미세역학 기반의 해석 (Ju and Chen, 1994) 과 Mesquita and Coda (2002)의 근사식을 사용하였다. 이를 통해 구한 재료 물성은 복합재료의 크리프 거동예측을 위한 Kelvin-Voight (KV) 모델과 Standard Linear Solid (SLS) 모델에 적용되었다. 최종적으로 본 연구에서 제안한 손상을 고려한 점탄성 모델의 예측과 시험결과를 비교 수행하여 결과의 타당성을 검증하였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.41 no.5
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• pp.342-349
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• 2013

A damage imposed on an unmanned aerial vehicle changes the flight dynamic characteristics, and makes difficult for a conventional controller based on undamaged dynamics to stabilize the vehicle with damage. This paper presents a neural network based adaptive control method that guarantees stable control performance for an unmanned aerial vehicle even with damage on the main wing. Additionally, Pseudo Control Hedging (PCH) is combined to prevent control performance degradation by actuator characteristics. Asymmetric dynamic equations for an aircraft are chosen to describe motions of a vehicle with damage. Aerodynamic data from wind tunnel test for an undamaged model and a damaged model are used for numerical validation of the proposed control method. The numerical simulation has shown that the proposed control method has robust control performance in the presence of wing damage.

• Computational Structural Engineering
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• v.10 no.4
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• pp.229-238
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• 1997

Mechanical behavior of asphalt concrete that accounts for viscoelasticity and damage evolution under cyclic loading conditions is modeled and presented in this paper. An elastic-viscoelastic correspondence principle in terms of pseudo variables is applied to separately evaluate viscoelasticity and time-dependent damage growth in asphalt concrete. A microcrack growth law, which is commonly employed in linear viscoelastic fracture mechanics, is successfully used for describing the damage growth in the body. A constitutive equation in terms of stress and pseudo strain is first established for controlled-strain mode, and then transformed to controlled-stress constitutive equation by simply replacing stress and pseudo strain with pseudo stress and strain. The transformed constitutive equation in terms of pseudo stress satisfactorily predicts the mechanical behavior of asphalt concrete all the way up to failure under controlled-stress modes.

• Tunnel and Underground Space
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• v.24 no.3
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• pp.187-200
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• 2014

After excavation or blasting, rock properties within an excavation damaged zone can be perpetually weakened on account of stress redistribution or blasting impact. In the present study, the excavation damaged zone is applied to a rock slope. The objective of this research is to compare the mechanical stability of the rock slope depending on the presence of the damaged zone using 2-dimensional modeling and analyze factors affecting factor-of-safety. From the modeling, it was founded that the mechanical stability of the rock slope is significantly dependent on the presence of the damaged zone. In particular, factor-of-safety with a consideration of the damaged zone decreased by approximately 49.4% in comparison with no damaged zone. Factor analysis by fractional factorial design was carried out on factor-of-safety. It showed that the key parameters affecting factor-of-safety are angle of the slope, cohesion, internal friction angle and height.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.28 no.1A
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• pp.115-123
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• 2008

The performance prediction of fiber-reinforced composites has attracted engineer's attention in many fields, and the various theoretical and numerical methods have been proposed to predict the behavior of the fiber-reinforced composites. An evolutionary damage model for progressive interfacial debonding between circular fibers and the matrix is newly incorporated into the micromechanics-based elastoplastic model proposed by Ju and Zhang (2001) in this framework. Using the proposed model, a series of numerical simulations are conducted to illustrate the elastoplastic behavior and evolutionary damage of the framework. Furthermore, the influence of the evolutionary interfacial debonding on the behavior of the composites is investigated by comparing it with the result of a stationary damage model.