• Title/Summary/Keyword: 두께비

Search Result 3,853, Processing Time 0.046 seconds

Thickness Assessment of Adhesive Layer in Inhomogeneous Layer by Guided Wave (유도초음파에 의한 비균질 적층의 접합층두께 평가)

  • Cho, Youn-Ho;Ham, Hyo-Sik;Choi, Heung-Ho
    • Journal of the Korean Society for Nondestructive Testing
    • /
    • v.21 no.4
    • /
    • pp.391-397
    • /
    • 2001
  • The guided wave propagation in inhomogeneous multi-layered structures is experimentally explored based on theoretical dispersion curves. It turns out that proper selection of incident angel and frequency is critical for guided wave generation in multi-layered structures. Theoretical dispersion curves greatly depend on adhesive zone thickness, layer thickness and material properties. It was possible to determine the adhesive zone thickness of an inhomogeneous multi-layered structure by monitoring experimentally the change of dispersion curves.

  • PDF

Hygrothermal Bending Analysis of Laminated Composite Plates and Shells Considering a Higher-order Shear Deformation (고차전단변형을 고려한 적층복합판 및 쉘의 열-습윤 휨해석)

  • 한성천;윤석호
    • Journal of the Computational Structural Engineering Institute of Korea
    • /
    • v.12 no.1
    • /
    • pp.37-44
    • /
    • 1999
  • 비등방성으로 적층된 복합판 및 쉘구조물에서 온도와 습도의 급격한 변화는 구조물의 강도와 성능을 저하시키는 중요한 원인이 된다. 더욱이 하중에 의한 역학적 변위와 조합될 때에는 좌굴, 대변형 혹은 고응력 상태를 유발하게 된다. 본 연구에서는 이중 퓨리에급수를 이용하여 3차의 전단변형함수로 가정된 평형방정석을 전개하고 폭-두께비, 형상비의 변화 그리고 재료의 성질에 따른 결과에 대하여 고찰하였다.

  • PDF

Thickness effect of electrical resistivity using Four Point Probe (Four Point Probe 방법을 이용한 전기비저항의 두께효과)

  • Kang, J.H.;Kim, H.J.;Yu, K.M.;Han, S.O.;Kim, J.S.;Park, K.S.;Ryu, J.C.
    • Proceedings of the KIEE Conference
    • /
    • 2006.07c
    • /
    • pp.1388-1389
    • /
    • 2006
  • 금속의 전기비저항 측정은 4단자 방법, van der Pauw 방법, Four Point Probe(FPP) 방법 등이 있으며, 이들의 정확한 측정방법을 고찰하고, 그 중 FPP 방법에 의한 비저항의 두께효과를 비교 분석하기 위하여 비자성 금속 SUS 316을 두께별로 가공한 후 실험하였다. 그 결과 4단자 및 van der Pauw 방법으로 측정된 도전율은 각각 2.273 %IACS으로 나타났으며, FPP방법으로 측정된 도전율은 probe spacing 5.0 mm, dc current 10 A에서 시료의 두께가 2 mm일 때 2.288 %IACS, 3 mm일 때 2.271 %IACS로서 상기 두 방법으로 측정한 결과와 0.5 %이내에서 일치하였으나, 시료가 5mm 및 11 mm 에서는 매우 큰 오차를 나타냈다.

  • PDF

Finite Element Post-buckling Analysis of Steel-Concrete Composite Column (철골-콘크리트 합성기둥의 후좌굴 거동에 관한 해석 연구)

  • Oh, Myoung Ho;Kim, Myeong Han;Kim, Sang Dae
    • Journal of Korean Society of Steel Construction
    • /
    • v.19 no.6
    • /
    • pp.725-735
    • /
    • 2007
  • The local buckling strength and post-local buckling strength of thin steel plates in the steel-concrete composite column were evaluated by nonlinear finite element analyses. The proposed width-to-thickness limit ratio was based on elastic buckling analyses, in which the increased local buckling capacity of the plate due to the in-filled concrete was considered by the boundary conditions of the thin plate. Considering the initial imperfections and residual stresses, we determined the initial local buckling strength and post-local buckling strength of the thin plates with various width-to-thickness ratios. The formula to evaluate the compressive capacity of the steel-concrete composite column based on the effective width of the plate was proposed. For verification, values determined by the formula were compared with the experimental results.

Derivations of Buckling Knockdown Factors for Composite Cylinders Considering Various Shell Thickness Ratios and Slenderness Ratios (다양한 두께비와 세장비를 고려한 복합재 원통 구조의 좌굴 Knockdown factor의 도출)

  • Kim, Do-Young;Sim, Chang-Hoon;Kim, Han-Il;Park, Jae-Sang;Yoo, Joon-Tae;Yoon, Young-Ha;Lee, Keejoo
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.49 no.4
    • /
    • pp.321-328
    • /
    • 2021
  • This paper derives numerically new buckling Knockdown factors for the lightweight design of the composite propellant tanks for space launch vehicles. A nonlinear finite element analysis code, ABAQUS, is used for the present postbuckling analysis of composite cylinders under compressive loads. Various thickness ratios (R/t) and slenderness ratios (L/R) are considered and Single Perturbation Load Approach is applied to represent the geometric initial imperfection of the composite cylinder. For the composite cylinder with thickness ratio of 500 and slenderness ratio of 2.04, the buckling Knockdown factor derived in this work is higher by 84.38% than NASA's previous buckling design criteria. Therefore, it is investigated that a lightweight design is possible when the present Knockdown factors are used for the design of composite propellant tanks. In addition, it is shown that global buckling loads and buckling Knockdown factors decrease as the thickness ratio or slenderness ratio of composite cylinders increases.

Hamrock & Dowson의 타원접촉 EHL 유막두께식에 대한 고찰

  • 박태조
    • Proceedings of the Korean Society of Tribologists and Lubrication Engineers Conference
    • /
    • 1995.06a
    • /
    • pp.31-36
    • /
    • 1995
  • 본 논문에서는 유한차분법과 뉴우튼-랍슨 방법을 사용하여 타원접촉 EHL 문제를 수치해석하고 그 결과를 H-D의 해석결과 및 그들의 유막두께식과 비교하였다. 최소유막의 크리 뿐만 아니라 중앙부의 유막두께도 H-D이ㅡ 결과와 차이를 보이며, 특히, 하중변화에 대한 중앙부 유막두께는 상당히 크게 차이를 나타내고 있다. 따라서 본 논문에서 구한 정확한 수치해석결과를 사용하면 H-D나 Chittenden 등의 유막두께식에 비하여 EHL 상태에서의 유막두께를 보다 정확하게 예측할 수 있는 새로운 유막두께식을 제시할 수 있을 것으로 생각되며 이를 위해서 추가적인 연구가 요구된다.

  • PDF

A Study on Vibration Characteristics of Plate Structures Spot-Welded with respect to Area Ratio and Distance Ratio (점용접된 판 구조물의 면적비와 거리비에 따른 진동특성 연구)

  • Han, Dong-Seop;Ahn, Sung-Chan;Ahn, Chan-Woo;Han, Geun-Jo
    • Journal of Navigation and Port Research
    • /
    • v.26 no.1
    • /
    • pp.43-49
    • /
    • 2002
  • In this Paper, the mechanical behavior of two reかangular plates spot-welded under free vibration is investigated in detail. The focus of the analysis is to evaluate the effect of thickness of reinforced plates with equivalent thickness. The results of this the investigation are compared with detailed finite element analysis end experiments of the plates spot-welded for various parameters, such as aspect ratio, arm ratio, and distance ratio of spot-welding Points. The conclusion obtained are as followed. 1. The effect thickness due to spot-weld is very large, such as 55% in comparison with area ratio of spot-welding joint is just 4.52%. 2 The effect of thickness with respect to the distance ratio is maximized when the distance ratio is 0.4.

Shear Strength of Plate Girder (플레이트거더의 전단내력)

  • Choi, Chui-Kyung;Kim, Kyu-Suk
    • Journal of the Korea institute for structural maintenance and inspection
    • /
    • v.7 no.2
    • /
    • pp.169-176
    • /
    • 2003
  • In the design of plate girder web panels, it is required to evaluate accurately the elastic buckling strength under shear, whether or not the post-buckling strength is accounted for. Currently, elastic shear buckling coefficient of web panels stiffened by transverse intermediate stiffeners are determined by assuming conservatively that web panels are simply supported at the juncture between the flange and web. Although the notion of the real boundary condition at the juncture of the web and the flanges to be somewhere between simple and fixed has been recognized from early days, the boundary condition has been conservatively assumed, mainly due to lack of means to evaluate it in a rational manner. In this paper, a series of numerical analyses and experiments is carried out to provide a simple equation with some parameters especially the flange-web thickness ratio.

Rotor Leading Edge Thickness Effect on Supersonic Impulse Turbine Performance (초음속 충동형 터빈의 로터 앞전 두께가 성능 변화에 미치는 영향)

  • Lee, Hang-Gi;Jung, Eun-Hwan;Park, Pyun-Gu;Kim, Jin-Han
    • Journal of the Korean Society of Propulsion Engineers
    • /
    • v.15 no.4
    • /
    • pp.41-47
    • /
    • 2011
  • Turbopump, which is a part of 75 ton open cycle liquid rocket engine has a super sonic impulse turbine. This paper investigated the leading edge thickness effect on the turbine performance experimently. Two rotors were tested with the different leading edge thickness. The ratios (rotor thickness to Pitch) are 1.9 and 1.4 times to 30 ton turbine rotor. As a result, a rotor with 1.4 times ratio had a 1.5% higher efficiency gain than a rotor with 1.9 times ratio. The pressure ratio with the maximum efficiency on the same rotational speed was increased to the full expansion ratio of nozzle.

Analysis of Subthreshold Swing for Ratio of Channel Length and Thickness of Asymmetric Double Gate MOSFET (비대칭 DGMOSFET의 채널길이와 두께 비에 따른 문턱전압이하 스윙 분석)

  • Jung, Hakkee
    • Journal of the Korea Institute of Information and Communication Engineering
    • /
    • v.19 no.3
    • /
    • pp.581-586
    • /
    • 2015
  • This paper has analyzed the variation of subthreshold swing for the ratio of channel length and thickness for asymmetric double gate MOSFET. The asymmetric double gate MOSFET has the advantage that the factors to control the short channel effects increase since top and bottom gate structure can be fabricated differently. The degradation of transport property due to rapid increase of subthreshold swing can be specially reduced in the case of reduction of channel length. However, channel thickness has to be reduced for decrease of channel length from scaling theory. The ratio of channel length vs. thickness becomes the most important factor to determine subthreshold swing. To analyze hermeneutically subthreshold swing, the analytical potential distribution is derived from Poisson's equation, and conduction path and subthreshold swing are calculated for various channel length and thickness. As a result, we know conduction path and subthreshold swing are changed for the ratio of channel length vs. thickness.