• 제목/요약/키워드: critical thickness

검색결과 911건 처리시간 0.024초

Curvilinear free-edge form effect on stability of perforated laminated composite plates

  • Zerin, Zihni;Basoglu, Muhammed Fatih;Turan, Ferruh
    • Structural Engineering and Mechanics
    • /
    • 제61권2호
    • /
    • pp.255-266
    • /
    • 2017
  • In this study, self-supporting roofing elements especially convenient for large-span structures such as stadium, airport terminal, mall, coliseum, etc. were examined with respect to critical buckling load. These elements were assumed as laminated composite plates and, variation of free-edge forms, cutout types and lamination configurations were used as design parameters. Based on the architectural feature and structural requirements, the effects of curvilinear free-edge form on critical buckling load were focused on in this research. Within this scope, 14 types of lamination configuration were specified according to various orientation angle, number and thickness of plies with a constant value of total plate thickness. Besides that, 6 different types of cutout and 3 different free-edge forms were determined. By combining all these parameters 294 different critical buckling load analyses were performed by using ANSYS Mechanical software based on finite element method. Effects of those parameters on critical buckling load were evaluated referring to the obtained results. According to the results presented here, it may be concluded that lamination conditions have more significant influence on the critical buckling load values than the other parameters. On the other hand, it is perceived that curvilinear free-edge forms explicitly undergo changings depending on lamination conditions. For future work, existence of delamination might be considered and progression of the defect could be investigated by using non-linear analysis.

Y$Ba_2$$Cu_3$$O_{7-x}$ 후막의 고속 증착과 임계 전류 밀도의 두께 의존성 (High-rate growth $YBa_2$$Cu_3$$O_{7-x}$ thick films and thickness dependence of critical current density)

  • 조월렴
    • Progress in Superconductivity
    • /
    • 제6권1호
    • /
    • pp.13-18
    • /
    • 2004
  • High-.ate in-situ$ YBa_2$Cu$Cu_3$$O_{7-x}$ (YBCO) film growth was demonstrated by means of the electron beam co-evaporation. Even though our oxygen pressure is low, ∼$5 ${\times}$10^{-5}$ Torr, we can synthesize as-grown superconducting YBCO films at a deposition rate of around 10 nm/s. Relatively high temperatures of around 90$0^{\circ}C$ was necessary in this process so far, and it suggests that this temperature at a given oxygen activity allows a Ba-Cu-O liquid formation along with an YBCO epitaxy. Local critical current density shows a clear correlation with local resistivity. Homogeneous transport properties with a large critical current density ($4 ∼ 5 MA/\textrm{cm}^2$ at 77K, 0T) are observed in top faulted region while it is found that the bottom part carries little supercurrent with a large local resistivity. Therefore, it is possible that thickness dependence of critical current density is closely related with a topological variation of good superconducting paths and/or grains in the film bodies. The information derived from it may be useful in the characterization and optimization of superconducting films for electrical power and other applications.

  • PDF

Fracture mechanics analysis of multipurpose canister for spent nuclear fuels under horizontal/oblique drop accidents

  • Jae-Yoon Jeong;Cheol-Ho Kim;Hune-Tae Kim;Ji-Hye Kim;Yun-Jae Kim
    • Nuclear Engineering and Technology
    • /
    • 제55권12호
    • /
    • pp.4647-4658
    • /
    • 2023
  • In this paper, elastic-plastic fracture mechanics analysis is performed to determine the critical crack sizes of the multipurpose canister (MPC) manufactured using austenitic stainless steel under dynamic loading conditions that simulate drop accidents. Firstly, dynamic finite element (FE) analysis is performed using Abaqus v.2018 with the KORAD (Korea Radioactive Waste Agency)-21 model under two drop accident conditions. Through the FE analysis, critical locations and through-thickness stress distributions in the MPC are identified, where the maximum plastic strain occurs during impact loadings. Then, the evaluation using the failure assessment diagram (FAD) is performed by postulating an external surface crack at the critical location to determine the critical crack depth. It is found that, for the drop cases considered in this paper, the principal failure mechanism for the circumferential surface crack is found to be the plastic collapse due to dominant high bending axial stress in the thickness. For axial cracks, the plastic collapse is also the dominant failure mechanism due to high membrane hoop stress, followed by the ductile tearing analysis. When incorporating the strain rate effect on yield strength and fracture toughness, the critical crack depth increases from 10 to 20%.

단면감소를 고려한 파이프의 좌굴에 관한 연구 (Buckling Analysis of Pipelines with Reduced Cross Section)

  • 최동호;고영찬;권순길;이종선
    • 대한토목학회논문집
    • /
    • 제33권3호
    • /
    • pp.865-873
    • /
    • 2013
  • 본 연구에서는 부식이나 보강재가 고려된 비균일한 두께를 가지는 파이프라인에 대하여 일정한 외압을 받을 때의 탄성 좌굴하중을 이론적으로 산정하였다. 길이가 매우 긴 원통형 쉘 구조물인 파이프라인을 단순한 링 구조물로 가정하였고, 고유함수를 유도하여 좌굴 임계하중을 산정하였다. 또한, 두께 변화와 두께가 감소된 구간의 범위에 따른 변수해석을 수행하였다. 이론식에 의해 산정된 좌굴 임계하중 결과를 유한요소해석 결과와 비교하여 검증하였고, 두 결과는 잘 일치함을 알 수 있었다.

Temperature dependent buckling analysis of graded porous plate reinforced with graphene platelets

  • Wei, Guohui;Tahouneh, Vahid
    • Steel and Composite Structures
    • /
    • 제39권3호
    • /
    • pp.275-290
    • /
    • 2021
  • The main purpose of this research work is to investigate the critical buckling load of functionally graded (FG) porous plates with graphene platelets (GPLs) reinforcement using generalized differential quadrature (GDQ) method at thermal condition. It is supposed that the GPL nanofillers and the porosity coefficient vary continuously along the plate thickness direction. Generally, the thermal distribution is considered to be nonlinear and the temperature changing continuously through the thickness of the nanocomposite plates according to the power-law distribution. To model closed cell FG porous material reinforced with GPLs, Halpin-Tsai micromechanical modeling in conjunction with Gaussian-Random field scheme are used, through which mechanical properties of the structures can be extracted. Based on the third order shear deformation theory (TSDT) and the Hamilton's principle, the equations of motion are established and solved for various boundary conditions (B.Cs). The fast rate of convergence and accuracy of the method are investigated through the different solved examples and validity of the present study is evaluated by comparing its numerical results with those available in the literature. A special attention is drawn to the role of GPLs weight fraction, GPLs patterns through the thickness, porosity coefficient and distribution of porosity on critical buckling load. Results reveal that the importance of thermal condition on of the critical load of FGP-GPL reinforced nanocomposite plates.

Influence of Manufacturing Errors on the Dynamic Characteristics of Planetary Gear Systems

  • Cheon, Gill-Jeong;Park, Robert G. er
    • Journal of Mechanical Science and Technology
    • /
    • 제18권4호
    • /
    • pp.606-621
    • /
    • 2004
  • A dynamic analysis using a hybrid finite element method was performed to characterize the effects of a number of manufacturing errors on bearing forces and critical tooth stress in the elements of a planetary gear system. Some tolerance control guidelines for managing bearing forces and critical stress are deduced from the results. The carrier indexing error for the planet assembly and planet runout error are the most critical factors in reducing the planet bearing force and maximizing load sharing, as well as in reducing the critical stress.

원통형 굽힘을 받는 적층판의 임계좌굴 하중 (Critical Buckling Loads of Laminated Composites under Cylindrical Bending)

  • 이수용
    • 항공우주시스템공학회지
    • /
    • 제1권4호
    • /
    • pp.28-36
    • /
    • 2007
  • This paper presents critical buckling loads of laminated composites under cylindrical bending. In-plane displacements are assumed to vary exponentially through plate thickness. The accuracy of this theory is examined for symmetric/antisymmetric cross-ply, angle-ply and unsymmetric laminates under cylindrical bending. Analytical solutions are provided to investigate the effect of transverse shear deformation on critical buckling loads of the laminated plates, and the results are compared with those obtained from the first-order shear deformation plate theory and the classical laminated plate theory.

  • PDF

Bonding between high strength rebar and reactive powder concrete

  • Deng, Zong-Cai;Jumbe, R. Daud;Yuan, Chang-Xing
    • Computers and Concrete
    • /
    • 제13권3호
    • /
    • pp.411-421
    • /
    • 2014
  • A central pullout test was conducted to investigate the bonding properties between high strength rebar and reactive powder concrete (RPC), which covered ultimate pullout load, ultimate bonding stress, free end initial slip, free end slip at peak load, and load-slip curve characteristics. The effects of varying rebar buried length, thickness of protective layer and diameter of rebars on the bonding properties were studied, and how to determine the minimum thickness of protective layer and critical anchorage length was suggested according the test results. The results prove that: 1) Ultimate pull out load and free end initial slip load increases with increase in buried length, while ultimate bonding stress and slip corresponding to the peak load reduces. When buried length is increased from 3d to 4d(d is the diameter of rebar), after peak load, the load-slip curve descending segment declines faster, but later the load rises again exceeding the first peak load. When buried length reaches 5d, rebar pull fracture occurs. 2) As thickness of protective layer increases, the ultimate pull out load, ultimate bond stress, free end initial slip load and the slip corresponding to the peak load increase, and the descending section of the curve becomes gentle. The recommended minimum thickness of protective layer for plate type members should be the greater value between d and 10 mm, and for beams or columns the greater value between d and 15 mm. 3) Increasing the diameter of HRB500 rebars leads to a gentle slope in the descending segment of the pullout curve. 4) The bonding properties between high strength steel HRB500 and RPC is very good. The suggested buried length for test determining bonding strength between high strength rebars and RPC is 4d and a formula to calculate the critical anchorage length is established. The relationships between ultimate bonding stress and thickness of protective layer or the buried length was obtained.

변환영역 해석법을 통한 콘크리트 도로 포장의 다축 차량 하중에 대한 응력 분포 분석 (Stress Distribution in Concrete Pavements under Multi-Axle Vehicle Loads Obtained Using Transformed Field Domain Analysis)

  • 김성민;심재수;박희범
    • 콘크리트학회논문집
    • /
    • 제18권5호
    • /
    • pp.695-702
    • /
    • 2006
  • 본 연구는 콘크리트 포장에 복륜 단축, 복륜 복축, 복륜 삼축 등 복륜 다축 차량 하중이 작용할 때 포장의 응력 분포와 최대 응력을 변환영역에서의 해석법을 이용하여 분석하였다. 우선 변환영역에서의 해석법을 이용한 결과와 유한요소법을 이용한 결과를 비교하여 해석법의 정확성을 파악하였다. 그리고 종방향과 횡방향을 따라 응력의 분포형태를 분석하고, 콘크리트 슬래브의 두께, 콘크리트 탄성계수, 지반 탄성계수 등이 응력 분포에 미치는 영향을 분석하였다. 또한 하중 접지면적과 연관된 하중 접지압의 변화에 따른 콘크리트 포장의 응력 분포도 분석하였으며 콘크리트 포장에서 최대 응력이 어느 위치에서 발생하는지에 대한 연구도 수행하였다. 연구 결과 다축 하중에 의한 콘크리트 포장의 최대 응력은 콘크리트의 탄성계수가 증가할수록, 슬래브의 두께가 감소할수록, 그리고 지반 탄성계수가 감소할수록 증가하였다. 이러한 변수 등이 변할 때 축수에 따른 최대 응력 비율의 변화는 대체적으로 미소하지만 지반 탄성계수가 작을 때는 축수가 증가 할수록 최대 응력 비율이 급격히 증가한다. 횡방향의 최대 응력 발생 위치는 일반적으로는 접지압이 증가하면 바깥쪽에서 안쪽으로 이동하며 콘크리트 탄성계수나 슬래브 두께가 증가하거나 지반 탄성계수가 감소할 때도 최대 응력 발생 위치는 바깥쪽에서 안쪽으로 이동한다. 종방향 상의 최대 응력 위치는 하중 접지압에 영향을 받지 않으며 단축과 복축 하중일 경우는 축의 위치이며 삼축 하중일 경우에는 콘크리트 탄성계수나 슬래브 두께가 증가하던지 또는 지반 탄성계수가 감소하면 최대 응력이 생기는 종방향 위치가 양쪽 바깥축에서 중간축의 위치로 바뀌게 된다.

Titanium Interlayer가 TiN 박막의 밀착특성에 미치는 영향 (The Effect of Titanium Interlayer on the Adhesion Properties of TiN Coating)

  • 공성호;김홍유;신영식;김문일
    • 열처리공학회지
    • /
    • 제5권1호
    • /
    • pp.1-12
    • /
    • 1992
  • In order to improve adhesive force of TiN film, we sputtered titanium as interlayer before TiN deposition by Plasma Enhanced Chemical Vapour Deposition. We observed changes of hardness and adhesion at a various thickness of titanium interlayer and also examined analysis. At the critical thickness of the titanium interlayer(about $0.2{\mu}$), adhesive force of TiN films were promoted mostly. But over the critical thickness, a marked reduction of adhesive force was showed, because of the internal stress of titanium interlayer. From AES analysis, the adhesion improvement of TiN films was mainly caused by nitrogen diffusion into titanium interlayer during TiN deposition process which relieved stress concentration at TiN coating-substrate interface.

  • PDF