• Title/Summary/Keyword: Compact Tension Specimen

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원공 결함을 갖는 CTS 시험편의 혼합모드 하중 하에서의 피로균열 전파거동 (Fatigue Crack Propagation Behavior in CTS Specimen Under Mixed-Mode Loading with Hole Defefects)

  • 송삼홍;신승만;이정무;서기정
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 춘계학술대회
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    • pp.137-142
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    • 2003
  • In this study, the propagation behavior of fatigue crack effected hole defects was investigated under mixed-mode I+II loading. To create mixed-mode stress field at crack tip, the compact tension shear (CTS) specimen and loading device were used in this tests. The propagation experiments of fatigue crack were performed by changing of the loading application angle(${\phi}$) and the distance(L) estimated from pre-crack tip to hole center located side by side by side with a pre-crack. As L changes, the variation for propagation aspect of fatigue crack, fatigue life and crack propagation rate were examined under mixed-mode loading. Under mixed-mode loading, the propagation rate of fatigue crack increased while the propagation direction changed dramatically because of the interference of hole defects.

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시뮬레이션 해석을 통한 소재 별 소형 인장 시험편의 내구성 및 강도 특성에 관한 연구 (A Study on Durability and Strength Properties of Compact Tension Specimen by Material through Simulation Analysis)

  • 이정호;조재웅
    • 예술인문사회 융합 멀티미디어 논문지
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    • 제8권3호
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    • pp.579-588
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    • 2018
  • 소재들에는 플라스틱 수지와 섬유 및 단일 금속 등으로 만들어진 소재들과 경량 특성들을 가지는 복합소재, 각 소재들의 장점들을 취합하여 내구성을 극대화시키는 방식의 이종재료 등이 있다. 본 연구에서는 경량 복합소재인 CFRP에 주목하여 단일 소재로서 보편적으로 쓰이는 소재들인 스테인리스 강, 알루미늄과의 강도 특성을 CFRP와 비교 및 분석하고, 데이터를 확보하기 위해 각 소재 별로 동일한 규격의 소형 인장 시험편(C-T specimen)을 설계하여 시뮬레이션 인장 해석 연구를 수행하였다. 연구 결과, CFRP 시험편 모델의 경우 최대 변형량은 약 0.0148mm, 최대 응력은 약 59.104MPa, 최대 변형률 에너지는 약 0.00529mJ로 나타났으며, 스테인리스 강 시험편 모델의 최대 변형량은 약 0.0106mm, 최대 응력은 약 42.22MPa, 최대 변형률 에너지는 약 0.002699mJ로 나타났고, 알루미늄 시험편 모델의 최대 변형량은 약 0.023mm, 최대 응력은 약 33.29MPa, 최대 변형률 에너지는 약 0.00464mJ로 나타나는 것을 확인할 수 있었다. 이와 같이 본 연구에서 도출한 데이터들을 향후 복합소재에 대한 연구에서 기초적인 데이터로서 활용하고자 하였다.

표준 CT시험편을 이용한 실배관 파괴저항 곡선 예측 (Estimation of the Fracture Resistance Curve for the Nuclear Piping Using the Standard Compact Tension Specimen)

  • 박홍선;허용;구재민;석창성;박재실
    • 대한기계학회논문집A
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    • 제33권9호
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    • pp.930-937
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    • 2009
  • The estimation method of the fracture resistance curve for the pipe specimen was proposed using the load ratio method for the standard specimen. For this, the calculation method of the load - CMOD curve for the pipe specimen with the common format equation(CFE) was proposed by using data of the CT specimen. The proposed method agreed well with experimental data. The J-integral value and the crack extension were calculated from the estimated load - CMOD data. The fracture resistance curve was estimated from the calculated J-integral and the crack extension. From these results, it have been seen that the proposed method is reliable to estimate the J-R curve of the pipe specimen.

강재의 피로균열전파율에 미치는 시험편 크기의 영향 (Effect of Specimen Size on Fatigue crack Growth Rate in Steels)

  • 안석화
    • 한국해양공학회지
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    • 제14권2호
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    • pp.99-105
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    • 2000
  • This paper describes the effect of specimen size on fatigue crack growth rate for the offshore structural high-tensile-strength steel BS4360 and machine structural steel SM45C. The purpose of the present study is to investigate the effect of stress ratio aspect ratio specimen width and specimen thickness of the fatigue crack growth behavior. Compact tension specimens with a LT orientation for BS4360 and SM45C steels were used, All testing was done at constant stress intensity factor range controlled fatigue crack growth condition. The investigation demonstrates that the fatigue crack growth rate is increased with increasing stress ratio and specimen thickness and is decreased with increasing specimen width. The fatigue crack growth rate is unaffected by aspect ratio until a/W=0.50 but is increased by increasing spect ratio from a/W=0.55.

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피로크랙전파율에 대한 시험편 두께의 영향 (The Effect of Specimen Thickness on the Fatigue Crack Propagation Rate)

  • 고성위;엄윤성
    • 수산해양기술연구
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    • 제24권1호
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    • pp.44-49
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    • 1988
  • 본 연구에서는 피로파괴에 영향을 주는 여러 인자중에서 우선 피로크랙전파에 대한 시험편 두께의 영향을 검토하기 위하여 최초 두께 25mm인 일반구조용 압연강재를 평면가공하여 두께 5, 10, 15, 20, 25mm인 CT 시험편을 가공한 후 인장-인장편진반 복피로시험을 행하여 실험한 결과 다음과 같은 결론을 얻었다. 1. 피로수명이 가장 짧게 나타나는 임의의 시험편 두께가 존재하며, 본 실험의 경우에는 두께 15m인 시험편의 경우 피로수명이 가장 짧게 나타났다. 2. 피로크랙의 발생은 두께가 두꺼운 시험편의 경우가 늦지만 피로크랙 성장은 두꺼운 시험편의 경우가 빠르게 나타났다. 3. 본 실험에서 paris시의 계수 m의 값은 절위는 1.98~4.59로서 시험편의 두께가 두꺼울수록 m의 값이 크게 된다.

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모드 II 하중을 받는 CTS 시험편의 피로균열 전파거동에 관한 실험적 연구 (An Experimental Study on the Fatigue Crack Propagation Behavior in CTS Specimen under Mode II Loading)

  • 송삼홍;이정무
    • 대한기계학회논문집A
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    • 제27권7호
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    • pp.1217-1226
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    • 2003
  • The purpose of this paper is to investigate fatigue crack behavior under shear(Mode II) loading. Various specimens and devices have been used in order to produce Mode II loading in fatigue experiments for shear crack propagation. But, there is not sufficient comparisons of experimental results between Mode II and others loading modes, because of characteristics of applied loads and specimens. So, compact tension shear(CTS) specimens were used in this paper to investigate the propagation behavior of Mode II by comparing the experimental results between loading modes. We firstly observed the characteristics which was showed in Mode II experiment using CTS specimens. The experimental results under Mode II loading were compared with fatigue crack behavior under Mode I and Mixed-mode I+II loading. The characteristics for initiation and propagation behavior under Mode II loading was investigated by such comparisons.

유한요소법에 의한 금속재료의 탄소성파괴인성 예측 (Prediction of Elastic-Plastic Fracture Toughness for Metallic Material using Finite Element Method)

  • 선동주;박명균;박세만;최영택
    • 한국가스학회지
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    • 제1권1호
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    • pp.95-100
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    • 1997
  • 금속재료의 탄소성파괴인성치 측정을 위해서 ASTM E399 시험법에 따라 단순 인장 시험편을 사용하여 유한요소해석을 하였으며 여기에서 얻어진 하중-균열개구변위 곡선을 이용하여 균열개시점을 찾고 이 점에서의 파괴인성치 $J_{IC}$를 구하였다. 탄소성 파괴인성치 J 값은 J 적분법 및 M. K. Tseng등에 의해서 제안된 계산식을 이용하여 구하였다. 해석된 값의 검증을 위해서 고강도 저합금강인 AISI 4130 재료를 이용한 기존 실험값과 비교하였으며 그 결과는 잘 일치함을 알 수 있다.

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Analytical methods for determination of double-K fracture parameters of concrete

  • Kumar, Shailendra;Pandey, Shashi Ranjan;Srivastava, A.K.L.
    • Advances in concrete construction
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    • 제1권4호
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    • pp.319-340
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    • 2013
  • This paper presents a comparative study on the double-K fracture parameters of concrete obtained using four existing analytical methods such as Gauss-Chebyshev integral method, simplified Green's function method, weight function method and simplified equivalent cohesive force method. Two specimen geometries: three point bend test and compact tension specimen for sizes 100-500 mm at initial notch length to depth ratios 0.25 and 0.4 are used for the comparative study. The required input parameters for determining the double-K fracture parameters are derived from the developed fictitious crack model. It is found that the cohesive toughness and initial cracking toughness determined using weight function method and simplified equivalent cohesive force method agree well with those obtained using Gauss-Chebyshev integral method whereas these fracture parameters determined using simplified Green's function method deviates more than by 11% and 20% respectively as compared with those obtained using Gauss-Chebyshev integral method. It is also shown that all the fracture parameters related with double-K model are size dependent.

크리프 균열 성장 실험을 위한 소성 변위 결정법 (Plastic Displacement Estimates in Creep Crack Growth Testing)

  • 허남수;윤기봉;김윤재
    • 대한기계학회논문집A
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    • 제30권10호
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    • pp.1219-1226
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    • 2006
  • The ASTM test standard recommends the use of the compact tension specimen for creep crack growth rates measurement. In the creep crack growth rate test, the displacement rate due to creep is obtained by subtracting the contribution of elastic and plastic components from the total load line displacement rate based on displacement partitioning method fur determining $C^*-integral$, which involves Ramberg-Osgood (R-O) fitting procedures. This paper investigates the effect of the R-O fitting procedures on plastic displacement rate estimates in creep crack growth testing, via detailed two-dimensional and three-dimensional finite element analyses of the standard compact tension specimen. Four different R-O fitting procedures are considered; (i) fitting the entire true stress-strain data up to the ultimate tensile strength, (ii) fitting the true stress-strain data from 0.1% strain to 0.8 of the true ultimate strain, (iii) fitting the true stress-strain data only up to 5% strain, and (iv) fitting the engineering stress-strain data. It is found that the last two procedures provide reasonably accurate plastic displacement rates and thus should be recommended in creep crack growth testing. Moreover, several advantages of fitting the engineering stress-strain data over fitting the true stress-strain data only up to 5% strain are discussed.