세미나 및 이벤트
Shell models which can use fully 3d constitutive equations
세미나 날짜
2004-09-22
작성자
임아주
작성일
2004-09-22
조회
1506
1. 제 목 : Shell models which can use fully 3d constitutive equations
2. 연 사 : Professor Bostjan Brank (University of Ljubljana, Slovenia)
3. 일 시: 2004년 9월 23일 (목) 14:00 ~ 15:00
4. 장 소 : 301동 1512호 세미나실
5. 내 용
Conventional shell models (e.g. of Reissner-Mindlin type) require condensation of 3d constitutive equations. This cannot be done in a case of more complex large strain hyperelastic and elasto-plastic constitutive relations. If one still wants to combine fully 3d constitutive equations with a shell model, the kinematics of conventional shell models needs to be refined. The following possible refined shell formulations will be discussed: (a) EAS (enhanced assumed strain) formulation which decomposes strains into compatible and incompatible parts, (b) EAS formulation which decomposes deformation gradient into compatible and incompatible parts, (c) refined shell formulation with seven displacement-like kinematic parameters, (d) a modified version of (c). Some numerical examples will be shown to validate each formulation.
6. 연사 경력 : 1982-1987 BS. Dept. of Civil Eng., Univ. of Ljubljana, Slovenia
1988-1991 MS. Dept. of Civil Eng., Univ. of Ljubljana, Slovenia
1991-1994 Ph.D. Univ. of Ljubljana, Slovenia & Univ. of Wales Swansea, UK
1999-현재 Assistant Professor, Dept. of Civil Eng, Univ. of Ljubljana, Slovenia
7. 문 의 : 기계항공공학부 조 맹 효 교수 (☎ 880-1693)
2. 연 사 : Professor Bostjan Brank (University of Ljubljana, Slovenia)
3. 일 시: 2004년 9월 23일 (목) 14:00 ~ 15:00
4. 장 소 : 301동 1512호 세미나실
5. 내 용
Conventional shell models (e.g. of Reissner-Mindlin type) require condensation of 3d constitutive equations. This cannot be done in a case of more complex large strain hyperelastic and elasto-plastic constitutive relations. If one still wants to combine fully 3d constitutive equations with a shell model, the kinematics of conventional shell models needs to be refined. The following possible refined shell formulations will be discussed: (a) EAS (enhanced assumed strain) formulation which decomposes strains into compatible and incompatible parts, (b) EAS formulation which decomposes deformation gradient into compatible and incompatible parts, (c) refined shell formulation with seven displacement-like kinematic parameters, (d) a modified version of (c). Some numerical examples will be shown to validate each formulation.
6. 연사 경력 : 1982-1987 BS. Dept. of Civil Eng., Univ. of Ljubljana, Slovenia
1988-1991 MS. Dept. of Civil Eng., Univ. of Ljubljana, Slovenia
1991-1994 Ph.D. Univ. of Ljubljana, Slovenia & Univ. of Wales Swansea, UK
1999-현재 Assistant Professor, Dept. of Civil Eng, Univ. of Ljubljana, Slovenia
7. 문 의 : 기계항공공학부 조 맹 효 교수 (☎ 880-1693)
