• Title/Summary/Keyword: 정적강도시험

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Evaluation of Dynamic Tensile Strength of HPFRCC According to Compressive Strength Level (압축강도 수준에 따른 HPFRCC의 동적충격 인장강도 평가)

  • Park, Gi-Joon;Kim, Won-Woo;Park, Jung-Jun;Moon, Jae-Heum;Kim, Sung-Wook
    • Journal of the Korea institute for structural maintenance and inspection
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    • v.22 no.3
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    • pp.31-37
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    • 2018
  • This study evaluates the dynamic tensile behavior of HPFRCC according to compressive strength levels of 100, 140 and 180 MPa. Firstly, the compressive stress-strain relationship of 100, 140 and 180 MPa class HPFRCC was analyzed. As a result, the compressive strengths were 112, 150 and 202 MPa, respectively, and the elastic modulus increased with increasing compressive strength. The static tensile strengths of HPFRCC of 100, 140 and 180 MPa were 10.7, 11.5 and 16.5 MPa, and tensile strength also increased with increasing compressive strength. On the other hand, static tensile strength and energy absorption capacity at 100 and 140 MPa class HPFRCC showed no significant difference according to the compressive strength level. It was influenced by the specification of specimen and the arrangement of steel fiber. As a result of evaluating the dynamic impact tensile strength of HPFRCC, tensile strength and dynamic impact factor of all HPFRCCs tended to increase with increasing strain rate from 10-1/s to 150/s. In the same strain rate range, the DIF of the tensile strength was measured higher as the compressive strength of HPFRCC was lower. It is considered that HPFRCC of 100 MPa is the best in terms of efficiency. Therefore, it is advantageous to use HPFRCC with high compressive strength when a high level of tensile performance is required, and it is preferable to use HPFRCC close to the target compressive strength for more efficient approach at a high strain rate such as explosion.

Static Strength of Composite Single-Lap Shear Joint Specimen Using Z-pinning Patch (Z-피닝 패치를 사용한 복합재 단일-겹침 전단 접합 시편의 정적강도)

  • Choi, Ik-Hyeon;Lim, Cheol-Ho
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.41 no.8
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    • pp.613-618
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    • 2013
  • In this paper a new concept on z-pinning technology named by authors as 'z-pinning patch' will be introduced, which advantage is easy application at manufacturing site of composite structures. Using the trial manufactured z-pinning patch, the z-pinned composite single-lap shear joint specimens were successfully manufactured and tested to check the improvement of joint strengths. The z-pin's material is stainless steel and its surface was machined as zagged shape and chemically corroded to improve joint force with composite materials.

Strength Evaluation of Bonded Dissimilar Materials by Using Stress Singularity Factor (응력특이성계수에 의한 이종 접합재료의 강도평가)

  • Jeong, Nam-Yong;O, Bong-Taek
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.20 no.7
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    • pp.2087-2096
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    • 1996
  • Recentrly advantages in composite and light weight material techniques have led to the increased use of bonded dissimilar materials such as ceramics/metal bonded joints, IC package, brazing, coating and soldering in the various industries. It is required to analyze the evaluation method of fracture strength and design methodology of bonded joints in dissimilar materials. Stress singularity according to changes of scarf angles for bonded scarf joints in dissimilar materials was investigated by the boundary element method and static experiments. In this paper, effect of the stress singularity factors at the interface edges of scarf joints on various dissmilar materials combinations were investigated by analysis of its stress and stress singularity index using 2-dimensional elastic program of boundary element method. And the variations of stress singularity index by changes for Young's modulus ratios of materials and scarf angles were investigated. Also, it is found that stress singularities at bonded interface edges are disappeared for certain combination of scarf angle in a pair of bonded dissimilar materials. As the results, it is proposed that the strength evaluation by using stress singularity factors, $\Gamma$, considering stress singularity at the interface edges of bonded dissimilar materials, is very useful.

The Minimum Lap-spliced Length of the Reinforcement in the Steam Curing UHPC Bridge Deck Slab Joint (UHPC 바닥판 증기양생 현장이음부의 최소철근겹침이음길이)

  • Hwang, Hoon-Hee;Park, Sung-Yong
    • Composites Research
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    • v.26 no.2
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    • pp.135-140
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    • 2013
  • The static test was performed to verify the effect of the joint in the UHPC bridge deck slab and the minimum lap-spliced length was presented. A total of six test members was fabricated to estimate the static behavior of the steam curing UHPC bridge deck slab joint by the four points bending test method. The lap-spliced joint type was expected to be not only simple but also efficient in UHPC structure because of the high bond stress of UHPC. Test results show that the decrease of maximum flexural strength was about 30% and the minimum lap-spliced length which behaved similar to the continued reinforcement in strength and ductility was 150 mm.

An Experimental study on Shear Resisting Effect of Reinforced Concrete Beams Filling-up Carbon Fiber Rod Plastic (CFRP-Rod로 전단 보강된 철근콘크리트 보의 전단거동에 관한 실험적 연구)

  • Kim, Young-Sik;Park, Sung-Moo
    • Proceeding of KASS Symposium
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    • 2005.05a
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    • pp.183-190
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    • 2005
  • The purpose of this study is to investigate experimentally the shear resisting behavior of the reinforced concrete beams strengthened with reinforcement materials(CFRP). Five specimens were manufactured and tested under, static monotonic loading. The main variables In the test were a space and volume of reinforcement. The test result indicated that the method of CFRP increase significantly the shear strength of a reinforced concrete beam

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Prediction Fracture Strength on Adhesively Bonded scarf Joints in Dissimilar Materials (이종재료의 경사접착이음에 대한 파괴강도의 예측)

  • 정남용
    • Journal of the Korean Society of Manufacturing Technology Engineers
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    • v.4 no.4
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    • pp.50-60
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    • 1995
  • Recently advantages joining dissimiliar materials and light weight material techniques have led to increasing use of structural adhesives in the various industries. Stress singulartiy occurs at the interface edges of adhesively bonded dissimilar materials. So it is required to analyze its stress singularity at the interface edges of adhesively bonded joints indissimilar materials. In this paper, the analysis method of stress singularity is studied in detail. Also, effects of the stress singularity at the interface edge of adhesively bonded scarf joints in combinations of dissimilar materials are investigated by using 2-dimensional elastic program of boundary element method. As the results, the strength evaluation method of adhesively bonded dissimilar materials using the stress singularity factor, $\Gamma$,is very useful. The fracture criterion, method of strength evaluation and prediction of fracture strength by the stress singularity factor on the adhesively bonded dissimilar materials are proposed.

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Static Flexural Behavior of GFRP Composite Rigmat (복합소재 리그매트의 정적 휨 거동)

  • Hong, Kee-Jeung;Keum, Moon-Seoung;Lee, Sung-Woo
    • Proceedings of the Computational Structural Engineering Institute Conference
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    • 2010.04a
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    • pp.18-21
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    • 2010
  • 현재 유전개발이 가속화 되고 있는 캐나다의 유전개발현장에서 진입도로용으로 사용하고 있는 목재 가도 매트를 대체하기 위해 고강도 경량 고내구성 특성을 갖는 복합소재 리그매트를 개발하였다. 기존에 본 연구진이 개발한 리그매트는 중차량의 반복하중에 취약한 거동을 보였으므로 이를 해결하기 위한 개선형 리그매트를 개발하였다. 개선형 리그매트의 구조안전성을 평가하기 위하여 단일데크의 강축 휨에 대한 해석 및 시험을 실시하여 휨 거동 특성을 조사하였다.

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An Experimental and Analytical Studies on the Mechanical Behavior of High Tension Bolted Joints with Oversize Hole (과대공을 갖는 고장력 볼트 이음부의 역학적 거동에 관한 실험 및 해석적 연구)

  • Lee, Seung Yong;Park, Young Hoon;Cho, Sun Kyu;Chang, Dong Il
    • Journal of Korean Society of Steel Construction
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    • v.10 no.3 s.36
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    • pp.355-367
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    • 1998
  • To evaluate the mechanical behavior and the compressive stress distribution in high tension bolted joints according to the size of bolt hole, the experimental and analytical studies are performed with enlarging bolt hole size. In experimental study, the static test is performed to measure the slip coefficient, and the fatigue test is also performed to evaluate the fatigue strength and failure pattern of fatigue crack. In analytical study, the compressive stress distribution is investigated by using the finite element analysis. From the result of experimental study, the slip coefficient and fatigue strength of the high tension bolted joints with oversize hole are not much different but somewhat it has decreased. These are because the size of bolt hole is larger than the holes of nominal size, therefore the width of clamping force is decreased and the compressive stress distribution area is smaller, this is certificated in the finite element analysis. In addition, the origin of fatigue crack in the oversize holes is closer to the hole than in the holes of nominal size, consequently it is investigated that the origin of fatigue crack is intimately associated with the compressive stress distribution which is formulated by the clamping force in both base metal and splice plate.

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Evaluation of Structural Safety of Polyethylene Boats by Drop Test Method (낙하시험에 의한 폴리에틸렌 보트의 구조 안전성 평가)

  • Lee, Sung-Riong;Kang, Gyung-Ju;Cho, Seok-Swoo
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.18 no.5
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    • pp.531-542
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    • 2017
  • The structural safety of small craft, such as steel ships and FRP ships, can be estimated using the measurement test of the hull plate thickness or the longitudinal bending strength test. A polyethylene boat is made using inexpensive HDPE and can be mass produced. The structural safety of a polyethylene boat cannot be guaranteed because a polyethylene boat hull is notspecified in the KR technical rules. The inspection procedure of sailing yachts and pleasure boats and drop test method of ISO standard 12215-5 propose the structural strength required for small crafts as the drop test height. Therefore, in this study, the drop test of a polyethylene boat hull was carried out based on the inspection procedure of a sailing yacht and pleasure boat and the drop test method of ISO standard 12215-5. The drop load was acquired by the drop acceleration ofa boat hull. Structural analysis and safety of a polyethylene boat were performed by the drop load and allowable stress criteria. The calculation results of the hull plate thickness by structural design specification of ISO standard 12215-5 showed that polyethylene boat hull was more than two times thicker than a steel ship hull and the boat hull determined by the inspection procedure of sailing yacht and pleasure boat and drop test method of ISO standard 12215-5 was more than 1.2 times thicker than the boat hull determined by structural design specification of ISO standard 12215-5. Therefore, inspection procedure of sailing yachts and pleasure boats and drop test method of ISO standard 12215-5 was much more conservative than the structural design specification of ISO standard 12215-5 and could be used as the structural design method of a polyethylene boat.

An Experimental Study on the Hybrid Composite Carbody Structure (하이브리드 복합재 철도차량 차체에 대한 시험적 연구)

  • Kim Jung-Seok;Jeong Jong-Cheol;Lee Sang-Jin
    • Composites Research
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    • v.18 no.6
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    • pp.19-25
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    • 2005
  • This paper has performed an experimental study on the hybrid composite carbody of Korean tilting railway vehicle. The hybrid composite carbody has the length of 23m and is comprised of a 40mm-thick aluminium honeycomb core and 2mm-thick woven fabric carbon/epoxy face sheet. In order to evaluate the structural behavior and safety of the hybrid composite carbody, the static load tests such as vertical load, end compressive load, torsional load and 3-point support load tests have been conducted. The test was performed under Japanese Industrial Standard (JIS) 17105 standard. from the tests, the maximum deflection was 12.3mm and the equivalent bending stiffness of the carbody was $0.81\times10^{14}\;kgf{\cdot}mm^2$. The maximum strain of the composite body was below $20\%$ of failure strain of the carbon/epoxy face sheet.