• 제목/요약/키워드: Structural stress approach

검색결과 418건 처리시간 0.023초

손상된 재료의 탄소성변형에 대한 운동학적 해석 (Kinematic Description of Damage-Elastoplastic Deformation)

  • 박대효;박용걸
    • 전산구조공학
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    • 제10권4호
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    • pp.131-142
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    • 1997
  • 본 논문에서는 4차 손상유효 tensor를 이용하여 유한 탄소성변형에 대한 운동학적인 손상해석이 소개된다. 이는 뼈대구조에서의 연속체 손상역학의 유효응력개념을 통하여 이루어진다. 소규모 변형율상태에만 적용할 수 있는 등가변형율 혹은 에너지법과는 달리 제안된 운동학적인 방법은 유효변형율과 유한변형율에 적용할 수 있는 소규모 변형상태에 있어서의 손상탄소성변형율 사이의 관계를 제공한다. 이는 실제 형상과 가상의 유효형상 모두에 대한 변형장의 운동학을 직접 고려하여 수행된다. 이 방법은 등가변형율이나 변형율 에너지 경우처럼 소규모 변형율에 한정되지 않으며, 유한변형율에 대한 에너지등가의 가정과 일치함을 보여준다. 본 논문에서는 손상이 탄소성영역에서 운동학적으로 표현되며, 손상유효 tensor는 2차 손상 tensor를 통해 손상을 운동학적 측정값이 항으로 특징지워진다.

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적층평판의 응력해석 향상을 위한 고전적 고차전단변형이론의 개선 (On the Modification of a Classical Higher-order Shear Deformation Theory to Improve the Stress Prediction of Laminated Composite Plates)

  • 김준식;한 장우;조맹효
    • 한국전산구조공학회논문집
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    • 제24권3호
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    • pp.249-257
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    • 2011
  • 본 논문에서는 고전적 고차전단변형이론(HSDT)을 이용한 복합재료 적층평판의 응력해석 개선기법을 소개한다. 횡방향 응력들에 대해서만 변분을 취하는 혼합변분이론(Mixed variational theorem)을 통하여 횡방향 전단 변형에너지를 개선하였다. 가정된 횡방향 전단응력은 면내 변위가 5차 다항식을 갖는 고차 지그재그 이론으로부터 구하였으며, 변위들은 고전적 고차전단변형이론의 변위장을 사용하였다. 이 과정을 통하여 얻어진 변형 에너지를 본 논문에서는 EHSDTM라고 명명하였으며, 이 이론을 통해 복합재 적층평판의 변위와 응력을 계산함에 있어서 HSDT와 비슷한 수준의 계산적 효율을 가지면서, 동시에 최소자승오차법에 따른 후처리 과정을 적용함으로써 변위와 응력의 두께방향 분포를 정확하게 예측할 수 있도록 개선하였다. 계산된 결과는 고전적 HSDT, 3차원 탄성해 등의 여러 결과들과 비교하여 검증하였다.

면외 워핑함수를 고려한 보 구조물의 기계 및 열응력 해석 (A Thermal Stress Analysis of Beams with Out-of-Plane Warping)

  • 정용민;김준식
    • 한국전산구조공학회논문집
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    • 제29권3호
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    • pp.229-235
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    • 2016
  • 본 논문에서는 기존에 개발된 생브낭의 원리를 이용한 응력개선방법에 부가적인 면외 워핑함수를 도입하여 후처리함으로써 기계 및 열응력을 개선할 수 있는 방법을 소개하였다. 열응력 예측이 중요한 문제로 다루어지고 있으며, 이에 따라 수많은 보이론들이 개발되어왔다. 일반적으로 고차이론들이 열응력 예측에 유용하다고 알려져 있지만, 자유도가 많아 계산과정이 복잡하다는 단점이 존재한다. 이러한 단점들을 보완하기 위해, 본 연구에서는 계산이 비교적 간단한 고전 보이론의 변위장에 면외 워핑함수를 부가적으로 도입하고 합응력 등가를 통해 후처리함으로써 보 구조물의 열응력을 정확하게 예측할 수 있는 방법을 제시하였다. 그리고 다양한 경계조건을 가지는 수치예제들을 통해 탄성해와 비교함으로써 그 정확도를 검증하고, 면외 워핑함수가 응력개선에 미치는 영향에 대해 분석하였다.

Cylindrical bending of laminated cylindrical shells using a modified zig-zag theory

  • Icardi, Ugo
    • Structural Engineering and Mechanics
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    • 제6권5호
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    • pp.497-516
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    • 1998
  • A relatively simple two-dimensional multilayered shell model is presented for predicting both global quantities and stress distributions across the thickness of multilayered thick shells, that is based on a third-order zig-zag approach. As for any zig-zag model, the layerwise kinematics is accounted for, with the stress continuity conditions at interfaces met a priori. Moreover, the shell model satisfies the zero transverse shear stress conditions at the upper and lower free surfaces of the shell, irrespective of the lay-up. By changing the parameters in the displacement model, some higher order shell models are obtained as particular cases. Although it potentially has a wide range of validity, application is limited to cylindrical shell panels in cylindrical bending, a lot of solutions of two-dimensional models based on rather different simplyfying assumptions and the exact three-dimensional elasticity solution being available for comparisons for this benchmark problem. The numerical investigation performed by the present shell model and by the shell models derived from it illustrates the effects of transverse shear modeling and the range of applicability of the simplyfying assumptions introduced. The implications of retaining only selected terms depending on the radius-to-thickness ratio are focused by comparing the present solutions to the exact one and to other two-dimensional solutions in literature based on rather different simplyfying assumptions.

MFC센서를 이용한 피로수명예측에 관한 연구 (A Study on Prediction of Fatigue Life using MFC Sensors)

  • 이지훈;오동진;김명현
    • Journal of Welding and Joining
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    • 제31권6호
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    • pp.32-36
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    • 2013
  • The large-scale structures have the possibility that there are defects such as cracks due to stress concentration caused by geometric discontinuities in the structure. In this respect, the assessment of fatigue life and the development of structural health monitoring(SHM) are very important. Fatigue design of structure is typically accomplished either using a set of stress cycle (S-N) data obtained from fatigue tests or using the fracture mechanics approach. The stress intensity factor(SIF) is required for the estimation of fatigue crack propagation life from the linear elastic fracture mechanics (LEFM) perspective. In this study, Macro Fiber Composie(MFC) sensor for the measurement of SIF of two dimensional cracks is used. The SIF based on the piezoelectric constitutive law and fracture mechanics are calculated. The measured values of the SIF are later used for the prediction of the crack propagation life. In this study, the measured value of the SIF and the fatigue life are compared with the theoretical results.

Response of lap splice of reinforcing bars confined by FRP wrapping: modeling approach

  • Thai, Dam Xuan;Pimanmas, Amorn
    • Structural Engineering and Mechanics
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    • 제37권1호
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    • pp.95-110
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    • 2011
  • This paper presents a tri-uniform bond stress model for predicting the lap splice strength of reinforcing bar at the critical bond splitting failure. The proposed bond distribution model consists of three zones, namely, splitting zone, post-splitting zone and yielding zone. In each zone, the bond stress is assumed to be constant. The models for bond strength in each zone are adopted from previous studies. Combining the equilibrium, strain-slip relation and the bond strength model in each zone, the steel stress-slip model can be derived, which can be used in the nonlinear frame analysis of the column. The proposed model is applied to derive explicit equations for predicting the strength of the lap splice strengthened by fiber reinforced polymer (FRP) in both elastic and post-yield ranges. For design purpose, a procedure to calculate the required FRP thickness and the number of FRP sheets is also presented. A parametric investigation was conducted to study the relation between lap splice strength and lap splice length, number and thickness of FRP sheets and the ratio of concrete cover to bar diameter. The study shows that the lap splice strength can be enhanced by increasing one of these parameters: lap splice length, number or thickness of FRP sheets and concrete cover to bar diameter ratio. Verification of the model has been conducted using experimental data available in literature.

Effects of In-role Behaviour Gap on Interpersonal Behaviours Focused on the Mediating Effect of Stress

  • Song, Gi-Ryung;Kim, Kyoung-Seok
    • 아태비즈니스연구
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    • 제12권4호
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    • pp.41-52
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    • 2021
  • Purpose - This study is to identify the relationship between the gap of in-role behaviour (IRB) on employee's interpersonal behaviour with the different perspective considering this behaviour as a social action that employees show in their work life, away from the perspective of conventional research that treats IRB as task performance. Design/methodology/approach - This study focus on the level of IRB gap that individuals have with their colleagues and its effect on the interpersonal behaviours such as helping and incivility instigation. The higher the level of difference, the more likely it would negatively affect their interpersonal behaviour through stress. The analysis was conducted on 250 employees of Korean companies through partial least squares structural equation modelling. Findings - The analysis shows that IRB gaps have a negative effect on employee's fully helping, and partly instigated incivility, in mediating stress. Implications based on the results of the study were presented in the conclusion. Research implications or Originality - The approaches and findings thus study showed are unique because most of existing studies have not tried to focus on the gap of in-role behaviour between employees and their colleagues. This study can give novels inspirations to other researchers in the related field.

Hard Landing이 항공기 구조물에 미치는 영향성 연구 (A Study of the Effects of Hard Landing on Aircraft Structure)

  • 오용규;심상기;신기수
    • 한국군사과학기술학회지
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    • 제14권5호
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    • pp.805-811
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    • 2011
  • Aircraft MLG and wing structures have been recognized as fatigue critical structures and exposed to the risk of fatigue crack initiation and propagation. Furthermore, these structures are frequently subjected to serious dynamic loading condition during a Hard Landing which may lead to their failure. Especially, structural integrity of MLG and wing components is decreased as the flight time increased because of the fatigue damage accumulated on the aircraft. In this study, the effects of Hard Landing on the MLG and wing components of aging aircraft were evaluated by using numerical approach. To achieve the aim, a finite element model has been developed and simulations were conducted by varying the landing conditions. As a result, it was revealed that the high stress concentration phenomenon was occurred at the lower Side Brace of MLG. Thereby, the intensified inspection for the lower Side Brace should be considered to prevent unexpected aircraft mishap.

Comparative study of factors influencing tension lap splices in reinforced concrete beams

  • Karkarna, Yakubu M.;Bahadori-Jahromi, Ali;Jahromi, Hamid Zolghadr;Bonner, Emily;Goodchild, Charles
    • Advances in concrete construction
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    • 제10권4호
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    • pp.279-287
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    • 2020
  • The practice of splicing reinforcing bars in reinforced concrete structures to manage insufficient bar length is a common approach, which is mainly due to transportation limitations on bar length. The splicing of reinforcing bars side by side offers a simple and economical solution to the problem of continuity. This paper examines the influence of different structural parameters such as concrete cover, lap splice length, shear links confinement and concrete strength on the lap splices based on an extensive experimental database of laps and anchorage. The current study shows that increasing the lap splices beyond 50Ø has no additional benefit for increasing its strength. The results also show that relative to the measured stress, specimens with larger concrete side covers shows higher splice stress compared to the samples with smaller concrete covers.

Axisymmetric analysis of multi-layered transversely isotropic elastic media with general interlayer and support conditions

  • Lee, J.S.;Jiang, L.Z.
    • Structural Engineering and Mechanics
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    • 제2권1호
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    • pp.49-62
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    • 1994
  • Based on the transfer matrix approach and integral transforms, a solution method is developed for the stress analysis of axisymmetrically loaded transversely isotropic elastic media with generalized interlayer and support conditions. Transfer functions (Green's functions in the transformed domain) are obtained in explicit integral form. For several problems of practical interest with different loading and support conditions, solutions are worked out in detail. For the inversion operation, an efficient technique is introduced to remedy the slow convergence of numerical integrals involving oscillating functions. Several illustrative examples are considered and numerical results are presented.