• 제목/요약/키워드: solid loads

검색결과 212건 처리시간 0.023초

일단고정 타단스프링으로 지지된 변단면 Beck 기둥의 임계하중 (Critical Loads of Tapered Beck's Columns with Clamped and Spring Supports)

  • 김석기;박광규;이병구
    • 한국전산구조공학회논문집
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    • 제19권1호
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    • pp.85-92
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    • 2006
  • 이 논문은 일단고정 타단스프링으로 지지된 변단면 Beck 기둥의 임계하중에 관한 연구이다. 기둥의 변단면을 중실 직사각형 단면을 갖는 선형 변단면으로 채택하고, Bernoulli-Euler보 이론을 이용하여 경사종동력이 작용하는 소위 Beck 기둥의 자유진동을 지배하는 상미분방정식과 경계조건을 유도하였다. 이 미분방정식을 수치해석하여 하중-고유진동수 곡선을 얻고 이로부터 발산임계하중 및 동요임계하중을 산출하였다. 수치해석의 결과로부터 변단면 형태, 경사변수 및 스프링 강성이 임계하중에 미치는 영향을 고찰하였다

우주발사체 발사 시 음향하중 저감을 위한 발사대 설계 (Design of launch pad for mitigating acoustic loads on launch vehicle at liftoff)

  • Tsutsumi, Seiji
    • 한국음향학회지
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    • 제39권4호
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    • pp.331-341
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    • 2020
  • 우주발사체는 발사 시 추진장치에서 발생하는 고강도 소음에 의한 음향하중의 영향을 받는다. 로켓소음은 발사체와 페이로드 내 전자 및 기계 부품의 손상 및 오작동을 유발할 수 있기 때문에 음향하중의 예측 및 저감은 설계에 있어 중요한 고려사항이다. 본 논문에서는 로켓 소음의 생성 및 발사대의 음향설계 기법에 대한 최신 연구동향을 논하였다. 특히, 새로운 발사대 설계 방법론의 예로서 일본 Epsilon 로켓 발사대의 개발과정을 기술하였다. 전산유체역학 모사 및 1/42 축소모형 실험을 통하여 설계된 발사대의 음향하중 저감 효과를 Epsilon 로켓의 실제 비행 데이터 분석을 통하여 검증하였다.

Temperature distribution of ceramic panels of a V94.2 gas turbine combustor under realistic operation conditions

  • Namayandeh, Mohammad Javad;Mohammadimehr, Mehdi;Mehrabi, Mojtaba
    • Advances in materials Research
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    • 제8권2호
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    • pp.117-135
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    • 2019
  • The lifetime of a gas turbine combustor is typically limited by the durability of its liner, the structure that encloses the high-temperature combustion products. The primary objective of the combustor thermal design process is to ensure that the liner temperatures do not exceed a maximum value set by material limits. Liner temperatures exceeding these limits hasten the onset of cracking which increase the frequency of unscheduled engine removals and cause the maintenance and repair costs of the engine to increase. Hot gas temperature prediction can be considered a preliminary step for combustor liner temperature prediction which can make a suitable view of combustion chamber conditions. In this study, the temperature distribution of ceramic panels for a V94.2 gas turbine combustor subjected to realistic operation conditions is presented using three-dimensional finite difference method. A simplified model of alumina ceramic is used to obtain the temperature distribution. The external thermal loads consist of convection and radiation heat transfers are considered that these loads are applied to flat segmented panel on hot side and forced convection cooling on the other side. First the temperatures of hot and cold sides of ceramic are calculated. Then, the thermal boundary conditions of all other ceramic sides are estimated by the field observations. Finally, the temperature distributions of ceramic panels for a V94.2 gas turbine combustor are computed by MATLAB software. The results show that the gas emissivity for diffusion mode is more than premix therefore the radiation heat flux and temperature will be more. The results of this work are validated by ANSYS and ABAQUS softwares. It is showed that there is a good agreement between all results.

Investigations on the influence of radial confinement in the impact response of concrete

  • Al-Salloum, Yousef;Alsayed, Saleh;Almusallam, Tarek;Ibrahim, S.M.;Abbas, H.
    • Computers and Concrete
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    • 제14권6호
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    • pp.675-694
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    • 2014
  • Annular and solid concrete specimens with different aspect ratios and static unconfined compressive strengths were studied for impact loading using SHPB test setup. Numerical simulations in LSDYNA were also carried out and results were validated. The stress-strain curves obtained under dynamic loading were also compared with static compressive tests. The mode of failure of concrete specimen was a typical ductile failure at high strain rates. In general, the dynamic increase factor (DIF) of thin solid specimens was higher than thick samples. In the numerical study, the variation of axial, hydrostatic and radial stresses for solid and annular samples was studied. The core phenomenon due to confinement was observed for solid samples wherein the applied loads were primarily borne by the innermost concrete zone rather than the outer peripheral zone. In the annular samples, especially with large diameter inside hole, the distribution of stresses was relatively uniform along the radial distance. Qualitatively, only a small change in the distribution of stresses for annular samples with different internal diameters studied was observed.

Mode Switching Smooth Control of Transient Process of Grid-Connected 400 Hz Solid-State Power Supply System

  • Zhu, Jun-Jie;Nie, Zi-Ling;Zhang, Yin-Feng;Han, Yi
    • Journal of Power Electronics
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    • 제16권6호
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    • pp.2327-2337
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    • 2016
  • The mode-switching control of transient process is important to grid-connected 400 Hz solid-state power supply systems. Therefore, this paper analyzes the principle of on-grid and islanding operation of the system with or without local loads in the grid-connected process and provides a theoretical study of the effect of different switching sequences on the mode-switching transient process. The conclusion is that the mode switch (MS) must be turned on before the solid-state switch (STS) in the on-grid process and that STS must be turned off before the MS in the off-grid process. A strategy of mode-switching smooth control for transient process of the system is proposed, including its concrete steps. The strategy utilizes the average distribution of peak currents and the smooth adjustment of peak currents and phases to achieve a no-shock grid connection. The simulation and experimental results show that the theoretical analysis is correct and that the method is effective.

새로운 개념의 복합재 샌드위치 체결부 구조의 설계와 검증 (Design and Verification of a Novel Composite Sandwich Joint Structure)

  • 곽병수;주현우;김홍일;동승진;권진회
    • Composites Research
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    • 제30권6호
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    • pp.384-392
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    • 2017
  • 인장과 압축하중 모두를 효과적으로 지지할 수 있는 새로운 샌드위치 체결부 구조의 설계를 위해, 체결부 형상이 다른 3가지 샌드위치 판넬에 대한 인장 및 압축 시험을 수행하였다. 샌드위치 판넬의 코어는 주로 알루미늄 플렉스 허니콤이지만, 타 구조물과의 체결을 위해 두께가 얇아지면서 단순 적층판으로 변하는 램프 영역에서는 PMI 폼 코어를 사용하였고, 면재에는 탄소섬유 복합재를 사용하였다. 형상 1에서는 복합재 플랜지와 샌드위치 구조가 일체형으로 연결된다. 형상 2와 3에서는 별도로 제작된 알루미늄 플랜지가 복합재 적층판에 하이록핀과 접착제로 체결된다. 시험 결과 형상 1, 2, 3의 평균 압축파손하중은 각각 295 kN, 226 kN, 291 kN으로 나타났고, 평균 인장파손하중은 각각 47.3(층간분리), 83.7 kN(볼트파손), 291 kN(치구손상)으로 나타났다. 압축 파손하중만을 고려할 경우 플랜지와 샌드위치 판넬을 복합재 일체형으로 제작한 형상 1과 3이 우수한 특성을 보였다. 그러나 형상 1의 경우 인장하중을 받을 때 낮은 하중에서 플랜지 모서리 부분에서 층간분리가 발생하였다. 따라서 인장과 압축하중을 동시에 효과적으로 지지할 수 있는 구조는 모서리에서 층간분리의 위험이 없게 별도의 알루미늄 플랜지를 사용하여 볼트로 체결한 형상 3임을 확인하였다.

가스압력용기의 응력거동특성에 관한 유한요소해석 (Finite Element Analysis of Stress Behaviour Characteristics in Gas Pressure Vessels)

  • 김청균;조승현
    • 한국가스학회지
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    • 제7권3호
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    • pp.58-64
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    • 2003
  • 본 연구에서는 압력용기의 안전설계에 대한 해석결과를 제시하고 있다. 압력용기에 가스압력과 온도하중이 동시에 작용할 경우, 응력과 변위량에 대한 해석적 연구를 수행하였다. 용기에 대한 설계는 ASME Sec. VIII Div. 2 code를 따라 설계하였다. 이 결과를 사용하여 열적 하중과 기계적 하중을 받는 압력용기를 FEM 해석기법으로 설계 안.전성을 검증하고자 한다. 유한요소해석 결과에 의하면, ASME 설계코드로 압력과 온도하중을 동시에 받는 경우를 해석한 데이터는 압력용기의 설계 안전성을 보장을 할 수 없을 것으로 예상된다. 또한, 압력용기 설계에서 일정한 두께를 갖는 일체형이 보강테를 설치한 압력용기보다 안전하다는 결과를 제시하고 있다.

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Numerical modelling for monitoring the hysteretic behaviour of CFRP-retrofitted RC exterior beam-column joints

  • Mahini, Seyed S.;Ronagh, Hamid R.
    • Structural Engineering and Mechanics
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    • 제38권1호
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    • pp.27-37
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    • 2011
  • This paper presents the results of a study on the capability of nonlinear quasi-static finite element modelling in simulating the hysteretic behaviour of CFRP and GFRP-retrofitted RC exterior beam-column joints under cyclic loads. Four specimens including two plain and two CFRP/GFRP-strengthened beam-column joints tested by Mahini and Ronagh (2004) and other researchers are modelled using ANSYS. Concrete in compression is defined by the modified Hognestad model and anisotropic multi-linear model is employed for modelling the stress-strain relations in reinforcing bars while anisotropic plasticity is considered for the FRP composite. Both concrete and FRP are modelled using solid elements whereas space link elements are used for steel bars considering a perfect bond between materials. A step by step load increment procedure to simulate the cyclic loading regime employed in the testing. An automatically reforming stiffness matrix strategy is used in order to simulate the actual seismic performance of the RC concrete after cracking, steel yielding and concrete crushing during the push and pull loading cycles. The results show that the hysteretic simulation for all specimens is satisfactory and therefore suggest that the numerical model can be used as an inexpensive tool to design of FRP-strengthened RC beam-column joints under cyclic loads.

Progressive collapse analysis of a RC building subjected to blast loads

  • Almusallam, T.H.;Elsanadedy, H.M.;Abbas, H.;Alsayed, S.H.;Al-Salloum, Y.A.
    • Structural Engineering and Mechanics
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    • 제36권3호
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    • pp.301-319
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    • 2010
  • The paper seeks to explore some aspects of the current state of knowledge on progressive collapse in the technical literature covering blast loads and structural analysis procedure applicable to reinforced concrete (RC) buildings. The paper describes the progressive collapse analysis of a commercial RC building located in the city of Riyadh and subjected to different blast scenarios. A 3-D finite element model of the structure was created using LS-DYNA, which uses explicit time integration algorithms for solution. Blast loads were treated as dynamic pressure-time history curves applied to the exterior elements. The inherent shortcomings of notional member removal have been taken care of in the present paper by simulating the damage of structural elements through the use of solid elements with the provision of element erosion. Effects of erosion and cratering are studied for different scenarios of the blast.

Long-term simulation of wind turbine structure for distributed loading describing long-term wind loads for preliminary design

  • Ibrahimbegovic, Adnan;Boujelben, Abir
    • Coupled systems mechanics
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    • 제7권2호
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    • pp.233-254
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    • 2018
  • In order to reduce the dependency on fossil fuels, a policy to increase the production capacity of wind turbine is set up. This can be achieved with increasing the dimensions of offshore wind turbine blades. However, this increase in size implies serious problems of stability and durability. Considering the cost of large turbines and financial consequences of their premature failure, it is imperative to carry out numerical simulations over long periods. Here, an energy-conserving time-stepping scheme is proposed in order to ensure the satisfying computation of long-term response. The proposed scheme is implemented for three-dimensional solid based on Biot strain measures, which is used for modeling flexible blades. The simulations are performed at full spatial scale. For reliable design process, the wind loads should be represented as realistically as possible, including the fluid-structure interaction (FSI) dynamic effects on wind turbine blades. However, full-scale 3D FSI simulations for long-term wind loading remain of prohibitive computation cost. Thus, the model to quantify the wind loads proposed here is a simple, but not too simple to be representative for preliminary design studies.