• 제목/요약/키워드: 3 point bending properties

검색결과 213건 처리시간 0.024초

유도무기 케이블 페어링의 강도 해석 및 접착재 강도 시험 (Bonding Stress Analysis of Cable Fairings used in Small Guided Missiles and Strength Tests of Bonding Materials)

  • 구남서;윤광준;신영석;이열화;정해용;김병화
    • 한국항공우주학회지
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    • 제33권6호
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    • pp.76-82
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    • 2005
  • 유도무기의 케이블 페어링은 공력하중 및 기계적 하중으로부터 전선 케이블을 보호하기 위하여 설치된다. 케이블 페어링을 설계하기 위해서는 유도무기 본체와 케이블 페어링 사이의 응력 분포가 필요하다. 본 연구에서는 케이블 페어링의 접착 응력 및 접착 강도 해석 기법을 고찰하여 프로그램화 하였다. 또한, 고온용 접착재에 대한 인장 시험과 3점 굽힘 시험을 통하여 강도를 계측하였고 이를 케이블 페어링의 설계에 적용하였다.

Numerical comparison between lattice and honeycomb core by using detailed FEM modelling

  • Giuseppe, Pavano
    • Advances in aircraft and spacecraft science
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    • 제9권5호
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    • pp.377-400
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    • 2022
  • The aim of this work is a numerical comparison (FEM) between lattice pyramidal-core panel and honeycomb core panel for different core thicknesses. By evaluating the mid-span deflection, the shear rigidity and the shear modulus for both core types and different core thicknesses, it is possible to define which core type has got the best mechanical behaviour for each thickness and the evolution of that behaviour as far as the thickness increases. Since a specific base geometry has been used for the lattice pyramidal core, the comparison gives us the opportunity to investigate the unit cell strut angle giving the higher mechanical properties. The presented work considers a detailed FEM modelling of a standard 3-point bending test (ASTM C393/C393M Standard Practice). Detailed FEM modelling addresses to detailed discretization of cores by means of beam elements for lattice core and shell elements for honeycomb core. Facings, instead, have been modelled by using shell elements for both sandwich panels. On lattice core structure, elements of core and facings are directly connected, to better simulate the additive manufacturing process. Otherwise, an MPC-based constraint between facings and core has been used for honeycomb core structure. Both sandwich panels are entirely built of Aluminium alloy. Prior to compare the two models, the FEM sandwich panel model with lattice pyramidal core needs to be validated with 3-point bending test experimental results, in order to ensure a good reliability of the FEM approach and of the comparison. Furthermore, the analytical validation has been performed according to Allen's theory. The FEM analysis is linear static with an increasing midspan load ranging from 50N up to 500N.

Bi/CNT 화합물과 Resin/CNT를 보강한 YBCO 초전도체의 기계적, 자기적 특성 변화 (Mechanical and Magnetic Properties of YBCO Superconductor with Bi/CNT Composite and Resin/CNT Impregnation)

  • 오원석;장건익;한영희;성태현
    • Progress in Superconductivity
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    • 제9권1호
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    • pp.107-110
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    • 2007
  • Bi/CNT composite and resin/CNT were chosen to improve the mechanical properties of $YBa_2Cu_3O_7$(YBCO) superconductor. In order to elucidate the effects of Bi/CNT composite and resin/CNT in YBCO superconductors, melt texture superconductor were impregnated by mixed compound of Bi and CNT into the artificial holes parallel to the c-axis, which were drilled on the YBCO superconductor. Various amount of Bi/CNT and resin/CNT were impregnated to YBCO superconductor with different holes diameters. Typical artificial holes diameters were 0.5, 0.7, and 1.0 mm respectively. Result of three-point bending test measurement, the bending strength with resin/CNT impregnation was improved up to 59.64 MPa as compared with 50.79 MPa of resin/CNT free bulk. Resin/CNT impregnation has been found to be one of the effective ways in improving the mechanical properties of bulk superconductor.

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굽힘하중을 받는 섬유 금속 적층판의 응력-변형률 예측을 위한 대변형 유한요소해석 (Finite Element Analysis of Large Deformation of Fiber Metal Laminates Under Bending for Stress-Strain Prediction)

  • 염경미;이종수
    • 대한기계학회논문집A
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    • 제39권10호
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    • pp.963-970
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    • 2015
  • 다양한 분야에서 금속 재료의 우수한 기계적 특성을 위해 경량화는 필수적이다. 최근에는 보다 효율적인 차체 경량화와 함께 내충격성 강화를 위하여 금속 부품 대신에 섬유 금속 적층판을 이용하는 연구가 활발히 진행되고 있다. 경량화를 위해서 자동차 및 항공기에서 복합재료나 샌드위치 구조로 이루어진 섬유 금속 적층판이 유용하다. 하지만, 섬유 금속 적층판 형태에 따른 기계적 특성이 도출되지 않은 실정이다. 본 논문에서는 적층판 두께 조합에 따른 특성 비교를 위하여 두께를 인자로 하고, 섬유 금속 적층판의 완전 요인 배치법으로 실험을 계획한다. 또한 유한요소 해석을 사용하여 알루미늄 판과 섬유 금속 적층판을 탄성과 소성 해석을 한다. 이를 통해 적층판 두께 조합에 따른 섬유 금속 적층판 형태에 따른 기계적 특성을 분석하고, 굽힘 대변형 거동을 예측하는 유한요소 해석모델을 구축한다.

유연 기판 위 적층 필름의 굽힘 탄성계수 측정 (Measurement of Flexural Modulus of Lamination Layers on Flexible Substrates)

  • 이태익;김철규;김민성;김택수
    • 마이크로전자및패키징학회지
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    • 제23권3호
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    • pp.63-67
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    • 2016
  • 본 논문에서는 폴리머 기반의 유연 기판 위 적층 된 다양한 필름의 굽힘 탄성계수의 간접 측정법을 소개한다. 패키징 기판의 다양한 적층 재료들의 탄성계수는 기계적으로 신뢰성 있는 전자기기 개발에 결정적이지만, 기판과 매우 견고히 접합하고 있는 적층 필름을 온전히 떼어 내어 자유지지형(free-standing) 시편을 만들기 어렵기 때문에 그 측정이 쉽지 않다. 이를 해결하기 위해 본 연구에서는 필름-기판의 복합체 시편에 대한 3점 굽힘을 진행하였고 시편 단면에 면적 변환법(area transformation rule)을 적용한 응력 해석을 수행하였다. 탄성계수를 알고 있는 기판에 대하여, 굽힘 시험으로 얻은 다층 시편의 강성으로부터 필름과 기판의 탄성계수 비를 계산하였으며, 전기 도금 구리 시편을 이용하여 양면 적층, 단면 적층의 두 가지 해석 모델이 실험 평가되었다. 또한 주요 절연체 적층 재료인 prepreg (PPG)와 dry film solder resist (DF SR)의 굽힘 탄성계수가 양면 적층 시편 형태로 측정 되었다. 결과로써 구리 110.3 GPa, PPG 22.3 GPa, DF SR 5.0 GPa이 낮은 측정 편차로 측정 됨으로써 본 측정법의 정밀도와 범용성을 검증하였다.

저속충격시험을 이용한 고체추진제의 동적 응력-변형률 특성 연구 (Study on the Dynamic Stress-Strain Behavior of Solid Propellant Using Low-Velocity Impact Test)

  • 황재민;고은수;조현준;김인걸;김재훈
    • 한국항공우주학회지
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    • 제49권10호
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    • pp.813-820
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    • 2021
  • 본 연구에서는 고체추진제의 동적 응력-변형률 특성을 고찰하기 위하여 저속충격시험을 수행하였다. 저속충격시험 시 충격체(Impactor)의 하중, 변위를 측정하여 고체추진제의 동적 거동을 확인하였다. 3점 굽힘 형태의 저속충격시험을 수행하였고, 이때 발생하는 국소변위와 길이가 짧고 두께가 두꺼운 고체추진제 시편의 전단 변위를 보상하여 순수 굽힘변위를 계산하였다. 보상된 변위와 측정된 하중을 사용하여 응력과 변형률을 계산하였고 응력-변형률 곡선으로부터 고체추진제의 동적 물성을 획득하여 이를 정적 굽힘 물성과 비교하였다. 운용 환경에 따른 온도별 고체추진제의 동적 물성을 획득하기 위해 상온, 고온, 저온에서 실험을 수행하고 결과를 비교분석하였다.

하이브리드 복합재료 튜브의 Pultrusion 성형공정연구 (A Study on the Pultrusion of Hybrid Composite Tube)

  • 성대영;김태욱;이광주
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 2001년도 춘계학술발표대회 논문집
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    • pp.180-183
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    • 2001
  • Glass fiber reinforced plastic(CFHP) tent pole fabricated by the pultrusion process with unidirectional glass fiber is two times as heavy as aluminum tent pole owing to the low specific modulus The first objective of this research is the design the high strength and light weight tent pole compete with. the second is the develope glass fiber carbon fiber hybrid tent pole pultrusion process. the third is the evaluate the mechanical properties of the hybrid tent pole compare to these of the duralumin tent pole.

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저농도 페놀수지 주입처리에 의한 평죽판 개발(1) (Development of Compressed-flattened Bamboo Impregnated with Low Molecular Weight PF Resin(1))

  • 이화형;김관의
    • 한국가구학회지
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    • 제12권2호
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    • pp.29-38
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    • 2001
  • This study was carried out to develope a new process of flattening bamboo pieces(3 months old) by two steps of utilizing microwave oven and hot press. Internode bamboo pieces were impregnated with low molecular weight phenol formaldehyde resin (PF) under vacuum of 76 cmHg, heated in a household microwave oven in 1 minute, pressed on the temperature of $145^{\circ}C$ by the hot press for 10 minute, and then cooled by the cold press in their flattened form. The physical and mechanical . Properties of compressed flattened bamboo were as follows: 1) PF1(Mw:427) and PF2(Mw:246) sol. met the success of flattening of internode bamboo pieces in both of P. bambusoides and P. nigra var. PF2 showed the more plasticity to flatten the bamboo than PFI. The PF2 sol. with low molecular weight(Mw:246) gave the more weight gain than that of PF1 in the equal concentration. PF1 of 5% (NVC) and PF2 of 10% (NVC) sol. gave the best result for physical and mechanical properties and from a economical view point. 2) The PFI of 5% (NVC) sol. with low molecular weight decreased the water absorption of 62-63% and increased the bending strength (MaR) of 80-90%, compression strength of 43-54%. 3) The PF2 of 10% (NVC) sol. with low molecular weight decreased the water absorption of 56-57% and increased the bending strength (MaR) of 64-86%, compression strength of 39-63%.

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Bending of a cracked functionally graded nanobeam

  • Akbas, Seref Doguscan
    • Advances in nano research
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    • 제6권3호
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    • pp.219-242
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    • 2018
  • In this study, static bending of an edge cracked cantilever nanobeam composed of functionally graded material (FGM) subjected to transversal point load at the free end of the beam is investigated based on modified couple stress theory. Material properties of the beam change in the height direction according to exponential distributions. The cracked nanobeam is modelled using a proper modification of the classical cracked-beam theory consisting of two sub-nanobeams connected through a massless elastic rotational spring. The inclusion of an additional material parameter enables the new beam model to capture the size effect. The new non-classical beam model reduces to the classical beam model when the length scale parameter is set to zero. The considered problem is investigated within the Euler-Bernoulli beam theory by using finite element method. In order to establish the accuracy of the present formulation and results, the deflections are obtained, and compared with the published results available in the literature. Good agreement is observed. In the numerical study, the static deflections of the edge cracked FGM nanobeams are calculated and discussed for different crack positions, different lengths of the beam, different length scale parameter, different crack depths, and different material distributions. Also, the difference between the classical beam theory and modified couple stress theory is investigated for static bending of edge cracked FGM nanobeams. It is believed that the tabulated results will be a reference with which other researchers can compare their results.

Effects of ceramic fillers on fracture resistance of barrier ribs of PDP

  • Baek, Se-Kyung;Kim, Yong-Seog
    • 한국정보디스플레이학회:학술대회논문집
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    • 한국정보디스플레이학회 2004년도 Asia Display / IMID 04
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    • pp.552-554
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    • 2004
  • Barrier ribs of plasma display panel (PDP) are glass matrix composite reinforced with alumina particles. Mechanical properties of the ribs are very crucial for the improvement in reliability of the panel as the ribs might fracture during transportation and service. In this study, therefore, the effects of filler type and content on the mechanical properties of the ribs were investigated. The fillers used include $Al_2O_3$, $TiO_2$, $ZrO_2$ and fused silica. The content of the filler was changed from 0 to 40 vol.%. The mechanical properties of the ribs measured were hardness, Young's modulus, fracture toughness, and 3-point bending modulus. The fracture toughness evaluated by micro-Vicker's indentation of the composites, in general, was measured to increase with the content of the filler until the sintered density does not decrease significantly. The improvement, however, was dependent on the type of filler employed.

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