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균일분포 온도하의 두꺼운 복합 재료 적층판의 열적 좌굴 해석
이영신,이열화,양명석,박복선,이종수,Lee, Young-Shin,Lee, Yeol-Wha,Yang, Myung-Seog,Park, Bock-Sun,Lee, Jong-Soo 대한기계학회 1993 대한기계학회논문집 Vol.17 No.7
In this paper, the thermal buckling of thick composite angle-ply laminates subject to uniform temperature distribution is studied. For the plates of 4-edges simply supported condition and those of 4-edges clamped condition, the critical buckling temperatue is derived, using tile finite element method based on the shear deformation theory. The effects of lamination angle, layer number, laminate thickness, plate aspect ratio and boundary constraints upon the critical buckling temperature are presented.
편마비 환자용 플라스틱 단하지보조기의 설계기술개발 (I) - 응력 해석을 통한 접근 -
이영신,최경주,조강희,임현균,Lee, Yeong-Sin,Choe, Gyeong-Ju,Jo, Gang-Hui,Im, Hyeon-Gyun 대한기계학회 2002 大韓機械學會論文集A Vol.26 No.1
In this study, a stress analysis is made fur an ankle foot orthosis (AFO) in the view point of structural stability. The investigated AFO is a solid and standard type. To analyze the stress distribution on the neck of AFO, the maximum AFO angular translation data is obtained by gait analysis. The material test of polypropylene is made to obtain the mechanical properties of AFO. The maximum dorsiflexion appears at the midstance in the gait analysis. The experimental angular translation at the top of AFO is about 10.3$^{\circ}$ at mid stance. Three models of AFO with different width of neck are made and analyzed with ABAQUS 6.1. The stress levels and distributions of 3 different width(W$_1$, W$_2$=0.85W$_1$, W$_3$=0.60W$_1$) AFO are investigated. As a result, the standard type(W$_1$) appears to the maximum stresses at the medial edge of cutout area surrounding ankle joint. The maximum stresses of the narrower type(W$_2$) are occured on medial edge and center of ankle. The narrowest type(W$_3$) appears to the maximum stresses at center of ankle. The maximum stresses become smaller as ankle width of AFO is narrower.
최대 열적 좌굴하중을 갖는 두꺼운 복합재료 적층판의 설계
이영신,이열화,양명석,박복선,Lee, Young-Shin,Lee, Yeol-Wha,Yang, Myung-Seog,Park, Bock-Sun 대한기계학회 1993 대한기계학회논문집 Vol.17 No.7
In this paper, the design of thick laminated composite plate subjected to thermal buckling load under uniform temperature distribution is presented. In the design procedures of composite laminated plates for maximum thermal buckling load. the finite element method based on shear deformed theory is used for the analysis or laminated plates. One-demensional search method is used to find optimal fiber orientation and, in the next step, optimal thickness is investigated. Design variables such as fiber orientation and ply thicknesses coefficient of plates are adopted. The optimal design for the symmetric or antisymmetric laminated plates consisted of 4 layers with maximum thermal buckling load is performed.
이영신,김용재,최영진,김월태,Lee Young-Shin,Kim Yong-Jae,Choi Young-Jin,Kim Wol-Tae 한국전산구조공학회 2005 한국전산구조공학회논문집 Vol.18 No.4
The cask is used to transfer the radioactive material in various fields required to withstand hypothetical accident condition such as 9m drop impact in accordance with the requirement of the domestic requlations and IAEA. So far the impact force has been obtained by the finite element method with complex computational procedure. In this study, the dynamic impact response of the cask body is analyzed using the mode superposition method, and the analysis method is proposed. The results we also validated by comparing with previous experimental results and finite element analysis results. The present method Is simpler than finite element method and can be used to predict the global impact response of cask 다양한 분야에서 방사선물질을 수송하기 위해 사용되고 있는 수송용기(cask)는 국내 원자력안전규정 및 IAEA 운반규정에서 정한 9m 자유낙하충격의 가상사고조건을 만족시켜야 된다. 현재까지 수송용기의 낙하충격력은 주로 복잡한 계산과정을 갖는 유한요소해석에 의해 수행되어 왔다. 본 논문에서는 수송용기 본체의 동적충격응답에 대해 모드중첩기법을 이용하여 해석하고 그 해법방법을 제시하였다. 해석결과는 이전에 실시되었던 시험결과와 유한요소해석과 비교를 통하여 그 타당성을 입증하였다. 본 해석방법은 유한요소 해석과 비교하여 간단한 방법으로서 수송용기에 대한 대체적인 동적응답을 예측할 수 있다.
이영신,최창,전병희,오재문,Lee, Young-Shin,Choi, Chang,Jun, Byoung-Hee,Oh, Jae-Moon 한국전산구조공학회 1997 전산구조공학 Vol.10 No.3
본 연구에서는 ANSYS와 ABAQUS 상용 유한요소 코드를 이용하여 궤도차량의 정적.동적 해석을 충격하중과 주행하중에 대해서 수행하였다. 궤도차량이 충격하중을 받을 때 최대 동적 Von Mises응력은 상판의 빔보강재와 레이스링사이에서 발생하였으며 응력수준은 390-450MPa이다. 정하중에 대한 동하중수 1.6을 고려했을 경우 동적 해석과 동적하중계수가 포함된 정하중 해석은 유사한 결과를 보이고 있다. 과도응력은 주로 레이싱링 주위에서 발생하고 있다. 주행하중의 경우 최대응력은 로드휠 유기압 현가장치 #1번에서 450MPa정도이며, 정적해석과 비선형 해석의 결과가 유사하다. In this study, static and dynamic transient analysis of tracked vehicle structure with recoil impact load is performed for transient impact and traveling load using ANSYS and ABAQUS FEM codes. When transient impact loads are applied at tracked vehicle, the maximum dynamic Von Mises stress occurs between beam stiffener of upper plate and race ring and stress level is about 390-450 MPa. The results of transient analysis shows similar level and tendency with static stress with dynamic force effect of 1.6. The excessive stresses occur around the race ring for the both cases. When the traveling loads are applied on the tracked vehicle, the maximum Tresca stress occurs around suspension #1 and is about 450 MPa and results of static and nonlinear transient analysis are quite similar.
이영신,이현,Lee, Young-Sin,Lee, Hyun 대한기계학회 1989 대한기계학회논문집 Vol.13 No.6
본 연구에서는 화이버각도, 경계조건 및 하중형태의 변화에 따라 적층 복합재료원통 셸 구조물의 수치예를 제시하고, NASTRAN수치결과 및 기존 문헌들과 비교하여 구하여진 결과의 타당성을 입증하였다.
고차 전단 변형이론에 의한 복합재료 적층판의 저속 충격응답
이영신,박웅,Lee, Young-Shin,Park, Oung 대한기계학회 1990 대한기계학회논문집 Vol.14 No.6
본 연구에서는 Kant 등이 제안한 고차판이론의 C연속변위 유한요소 모델을 사 용하여 충격자와 적층판의 저속 충격 응답에 대하여 연구하여 그 결과를 Mindlin의 판 이론에 의한 계산 결과와 비교하고, 경계 조건의 영향 및 충격자의 충격속도, 질량변 화에 대한 접촉력의 변화를 고찰하고자 한다. A $C^{0}$ continuous displacement finite element method based on a higher-order shear deformation theory is employed in the prediction of the transient response of laminated composite plates subjected to low-velocity impact. A modified contact law was applied to calculate the contact force during impact. The discrete element chosen is a nine-noded quadrilateral with 5 degree-of-freedom per node. The Wilson-.theta. time integration algorithm is used for solving the time dependent equations of the impactor and the central difference method was adopted to perform time integration of the plate. Numerical results, including the contact force history, deflection, and velocity history, are presented. Comparisons of numerical results using a higher order theory and a first-order theory show that using a higher order theory provides more accurate results. Effects of boundary condition, impact velocity, and mass of the impactors are also discussed.d.
이영신,류충현,명창문,Lee, Yeong-Sin,Ryu, Chung-Hyeon,Myeong, Chang-Mun 대한기계학회 2001 大韓機械學會論文集A Vol.25 No.9
The evolutionary structural optimization(ESO) method has been under continuous development since 1992. The bidirectional evolutionary structural optimization(BESO) method is made of additive and removal procedure. The BESO method is very useful to search the global optimum and to reduce the computational time. This paper presents the ranked bidirectional evolutionary structural optimization(R-BESO) method which adds elements based on a rank, and the performance indicator which can estimate a fully stressed model. The R-BESO method can obtain the optimum design using less iteration number than iteration number of the BESO.