• 한국농공학회지
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• 제40권5호
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• pp.91-99
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• 1998

The widespread use of thin shell structures has created a need for a systematic method of analysis which can adequately account for arbitrary geometric form and boundary conditions as well as arbitrary general type of loading. Therefore, the stress and analysis of thin shell has been one of the more challenging areas of structural mechanics. A wide variety of numerical methods have been applied to the governing differential equations for spherical and cylindrical structures with a few results applicable to practice. The analysis of axisymmetric spherical shell is almost an every day occurrence in many industrial applications. A reliable and accurate finite element analysis procedure for such structures was needed. Dynamic loading of structures often causes excursions of stresses well into the inelastic range and the influence of geometry changes on the response is also significant in many cases. Therefore both material and geometric nonlinear effects should be considered. In general, the shell structures designed according to quasi-static analysis may fail under conditions of dynamic loading. For a more realistic prediction on the load carrying capacity of these shell, in addition to the dynamic effect, consideration should also include other factors such as nonlinearities in both material and geometry since these factors, in different manner, may also affect the magnitude of this capacity. The objective of this paper is to demonstrate the dynamic characteristics of spherical shell. For these purposes, the spherical shell subjected to uniformly distributed step load was analyzed for its large displacements elasto-viscoplastic static and dynamic response. Geometrically nonlinear behaviour is taken into account using a Total Lagrangian formulation and the material behaviour is assumed to elasto-viscoplastic model highly corresponding to the real behaviour of the material. The results for the dynamic characteristics of spherical shell in the cases under various conditions of base-radius/central height(a/H) and thickness/shell radius(t/R) were summarized as follows : The dynamic characteristics with a/H. 1) AS the a/H increases, the amplitude of displacement in creased. 2) The values of displacement dynamic magnification factor (DMF) were ranges from 2.9 to 6.3 in the crown of shell and the values of factor in the mid-point of shell were ranged from 1.8 to 2.6. 3) As the a/H increases, the values of DMF in the crown of shell is decreased rapidly but the values of DMF in mid-point shell is increased gradually. 4) The values of DMF of hoop-stresses were range from 3.6 to 6.8 in the crown of shell and the values of factor in the mid-point of shell were ranged from 2.3 to 2.6, and the values of DMF of stress were larger than that of displacement. The dynamic characteristics with t/R. 5) With the thickness of shell decreases, the amplitude of the displacement and the period increased. 6) The values of DMF of the displacement were ranged from 2.8 to 3.6 in the crown of shell and the values of factor in the mid-point of shell were ranged from 2.1 to 2.2.

• 한국농공학회지
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• 제40권3호
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• pp.113-121
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• 1998

The widespread use of thin shell structures has created a need for a systematic method of analysis which can adequately account for arbitrary geometric form. Therefore, the stress analysis of thin shell has been one of the more challenging areas of structural mechanics. The analysis of axisymmetric spherical shell is almost an every day occurrence in many industrial applications. A reliable and accurate finite element analysis procedure for such structures was needed. In general, the shell structures designed according to quasi-static analysis may fail under conditions of dynamic loading. For a more realistic prediction on the load carrying capacity of these shell, in addition to the dynamic effect, consideration should also include other factors such as nonlinearities in both material and geometry since these factors, in different manner, may also affect the magnitude of this capacity. The objective of this paper is to demonstrate the dynamic characteristics of spherical Shell. For these purpose, the spherical shell subjected to uniformly distributed step load was analyzed for its large displacements elasto-viscoplastic dynamic response. The results for the dynamic characteristics of spherical shell in the cases under various conditions of base-radius/central height(a/H) and thickness/shell radius(t/R) were summarized as follows: 1. The dynamic characteristics with a/H, 1) As the a/H increases, the amplitude of displacement increased. 2) The values of displacement Dynamic Magnification Factor (DMF) range from 2.9 to 6.3 in the crown of shell and the values of factor in the mid-point of shell range from 1.8 to 2.6. 3) As the a/H increases, the values of DMF in the crown of shell is decreased rapidly but the values of DMF in mid-point of shell is increased gradually. 4) The values of DMF of hoop-stresses range from 3.6 to 6.8 in the crown of shell and the values of factor in the mid-point of shell range from 2.3 to 2.6, the values of DMF of stress were larger than that of displacement. 2. The dynamic characteristics with t/R, 1) With the decrease of thickness of shell decreses, the amplitude of the displacement and the period increased. 2) The values of DMF of the displacement were range from 2.8 to 3.6 in the crown of shell and the values of factor in the mid-point of shell were range from 2.1 to 2.2.

• 콘크리트학회논문집
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• 제19권1호
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• pp.121-130
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• 2007

본 연구에서는 FRP(fiber reinforced polymer) 합성재료에 의하여 콘크리트를 구속할 시 예상되는 콘크리트의 강도 및 변형 능력의 향상 효과를 알아보기 위하여 섬유 량 혹은 방향, 단부하중조건에 따른 wrap 혹은 튜브형의 구속형태, 반원형 쉘 및 수직 이음부의 유무에 따른 연속 및 불연속 구속 형태 등을 주요 변수로 한 총 36개의 원형단주 시험체에 대하여 단조가력 실험을 수행하였다. 여러 구속 방법에 따른 FRP의 파단변형률에 대하여서도 주의를 가지고 조사하였다. 구속된 콘크리트의 최대 강도 및 변형률을 산정하기 위하여 기존에 제시된 다양한 배경의 예측 식들에 대하여 검토하였으며, 이들에 의한 예측치와 실험치를 비교, 분석하였다. 구속되지 알은 콘크리트와 비교하여, CW 및 CF형은 매우 큰 강도 및 변형능력의 증가를 나타냈으며, 수직 이음부를 갖는 CP형은 폭발적으로 파괴하였으며, 보다 작은 강도 및 변형능력의 증가가 관측되었다. 대체로, 모든 시험체는 2선 선형관계의 응력-변형률 거동을 나타냈으며, 후반부의 변형경화 정도는 구속매체의 강성에 따라 결정되었다. 모든 시험체에서 관측된 FRP의 파단변형률은 인장시험편으로부터 획득한 극한변형률보다 정도에 따라서는 매우 작았다. 대체로, 기존 예측식들은 본 실험의 최대 강도 및 변형률을 과대평가 하였으며, 변형률 예측은 매우 산란된 분포를 나타냈다. 또한, 본 연구의 실험 결과에 근거하여 구속 콘크리트의 최대 강도 및 변형률을 보다 정확하게 예측할 수 있는 설계 목적의 단순식을 제안하였다. 강도식은 모어-쿨롱 파괴 기준을 사용하여 유도하였으며, 변형률식은 비구속 콘크리트를 주요 영향 요소로 포함하여 실험 결과를 fitting하였다./TEX> = 분광광도법으로 측정한 점토함량(%); $x_2$ = 유기물 함량($g{\cdot}kg^{-1})$)이었으며, 상관계수는 $0.984^{**}$로 두 방법사이에 높은 상관관계가 있는 것으로 조사되었다. 여기서 유도된 회귀방정식을 프로그램화하여 컴퓨터나 분석기기에 입력시 시간과 공간을 절약하고 신속하고 정확하게 점토함량을 분석할 수 있을 것으로 판단된다.119>잠118>잠107>잠117>잠113 순이었고, 웅견층중에서는 잠114>잠108>잠120>잠117>잠118>잠107>잠119>잠119>잠113 순이었다. 자견층 비율에서는 광의의 귀전력이 협의의 귀전력보다 컸고, 웅견층 비율에서는 같았다, 견층 비율에서는 일반조합 능력은 크게 나타났으나, 특정조합 능력과 상반조직 능력은 나타나지 않았다. 자견층 비율에서 교배친의 우성효과는 컸다. 자견층 비율에서는 교배친의 우성효과는 적었다. 자웅견층 비율의 잡종 강세는 적게 나타났다. 환경변이와 상가적 작계는 자웅견층 비율에서는 크게 나타났다. 우성의 방향은 자견층 비율에서는 정의 방향으로 우성 귀전자가 크게 작용하였으며, 자견층 비율에서는 정의 방향으로 우성 귀전자가 부분적으로 작용하였다. 교배친의 자견층 비율의 우성순서는 잠117>잠114>잠108>잠120>잠118>잠119>잠107>잠113 순이었고, 자견층 비율에서는 잠114>잠117>잠108>잠118>잠107>잠119>잠113>잠120의 순이었다.지방산의 조성이 많은 차이를 보였다.{2+}$ 26 및 $Na^+$ 26 mg $L^{-1}$이었다. 양액 재배 후 버려지는 폐양액 중의 무기성분 함량은