• 한국생산제조학회지
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• 제8권1호
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• pp.119-125
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• 1999

The distribution of fatigue crack growth rate is subjected to the measuring interval and calculated method of growth rate. In this paper, in order to establish the method of determining the distribution of fatigue crack growth rate, which ignores those influences, a series of fatigue crack growth experiments and measuring intervals of crack length calculated reasonable are presented. The main conclusions obtained are summarized as follows: 1) As a result of the ΔP constant test and ΔK constant test, it is thought that an approximate measuring interval of 0.3~0.7mm is reasonable, which allows for few errors and is little subjected to the calculated method of crack growth rate. 2) After generally comparing the error estimation by using the experimental data of CCT specimen with the error rating of the CT specimens, it is possible that the fatigue test has few errors within the measuring interval, ξ(Δa/W)=0.0067~0.017, regardless of the dimension of specimen geometry.

• Journal of the Korean Wood Science and Technology
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• 제43권6호
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• pp.861-867
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• 2015

유리섬유 보강적층재의 파괴인성을 평가하기 위하여 Compact tension (CT)형 시험을 실시하였다. 보강재는 직물형 유리섬유와 시트형 유리섬유강화플라스틱을 사용하였으며, 보강적층재는 층재사이에 보강재를 삽입 적층하였다. ASTM D5045에 의거하여 CT형 시험편을 제작하였다. 시험편의 길이는 끝면거리를 고려하여 선정하였으며, 인위적인 노치 끝에 볼트구멍(12 mm, 16 mm, 20 mm)을 선공하였다. 시트형 유리섬유강화플라스틱 보강적층재의 파괴인성하중은 보강하지 않은 적층재보다 최대 33% 증가하였으며, 직물형 유리섬유 보강적층재는 최대 152% 증가하였다. 이중외팔보(Double Cantilever Beam)이론에 의한 응력확대계수는 시트형 유리섬유강화플라스틱 보강적층재의 경우 1.08~1.38이었으며, 직물형 유리섬유 보강적층재는 1.38~1.86이었다. 이는 직물형 유리섬유 보강적층재의 경우 유리섬유와 층재의 섬유배열방향이 직교하여 파괴하중으로 인한 목재의 할렬진행을 억제시켰기 때문이다.

• 대한치과보철학회지
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• 제39권6호
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• pp.682-697
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• 2001

This investigation evaluated the fracture toughness($K_{IC}$) of eight currently available core materials, and relate the fracture toughness value to fractography analysis and surface characteristics using a atomic force microscope (AFM). Single-edge notched (SEN) test specimens (n=10) and compact tension (CT) test specimens (n=10) were prepared conforming to the ASTM Standard E-399 for a high copper amalgam, three composite core materials (Core-Max II, Core Paste, Bisfil Core), two reinforced composite core materials (Ti-Core, Ti-Core Natural), a resin-modified glass ionomer core material (Vitremer), and a conventional glass ionomer core material (Ketac-Molar). The specimens were tested with an Instron Universal Testing Machine. The maximum loads were measured to calculate the fracture toughness ($K_{IC}$). Thereafter, fracture surfaces of SEN specimens of each material were investigated for fractography analysis using scanning electron microscope. And, disc-shaped specimens with 1mm thickness were fabricated for each material and were investigated under AFM for surface morphology analysis. The results were as follows: 1. Bisfil Core showed the highest mean fracture toughness regardless of test methods. 2. For the tooth-colored materials, Ti-Core Natural exhibited the highest fracture toughness. 3. Ketac Molar showed a significantly low fracture toughness when compared with the amalgam and the composite resin core materials(p<0.05). 4. The fracture toughness values obtained with the single-edge notched test, except Ketac Molar, were higher than those obtained in the compact tension test. 5. SEM revealed that the fracture surface of high fracture toughness material was rougher than that of low fracture toughness material. 6. AFM revealed that the surface particles of the composite resins were smaller in size, with a lower surface roughness than the glass ionomer core materials.

• 한국정밀공학회지
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• 제7권4호
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• pp.130-139
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• 1990

It is well known that mechanisms of fracture and crack growth depend upon material characteristics such as fracture toughness, environmental condition, crack geometry and mechanical properties. It seems to be very important to investighate the effects of the above factors on the behavior of structural components which contain flaws for the detailed evaluation of their integrity. In this experimental research, fracture behaviors of SK-5 high carbon steel was investigated by using Acoustic Emission(AE) technique. Fracturing processes of materials were estimated through both the tension test with nominal specimens and the fracture test with compact tension specimens. The critical applied load which corresponds to the crack initiation and propagation is very improtant for the determination of yield strength of fracture toughness. The critical applied load($P_Q$) was determined through AE method and the source of AE signal was estimated by fractography analysis. The experimental results may contribute to the safety analyses and strength evaluation of structures.

• 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.

• 한국안전학회지
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• 제7권1호
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• pp.65-72
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• 1992

Objective of this research is to evaluate fracture behaviors of fresh-butt welded metal by the acoustic emission technique. The specimens used are medium carbon steel(SM45C), mild steel (SS41) and stainless steel(SUS304), which have different weldability. The similar welding and dissimilar welding processes are considered, in the former SM45C, SS41 and SUS304 are used, in the later the following metals are used SM45C and SS41, SM45C and SUS304 and SS41 and SUS304. The characteristics of fracture in weld metal are eshmated by the tension test with nominal speciemns, the fracture toughness test with compact tension specimens and fractography analysis. The results of tension test show for base metals and similar welding materials that the yield strength and ultimate strength of similar welding materials are increased, the elongation of those are decreased. The weldability of SUS304 is better than that of SM45C and SS41 In similar welding materials. Mechanical properties of dissimilar welding mateiiths we lower than those of similar welding materials. In dissimilar welding materials, the weldability of SM45C and SUS304 is better than that of SM45C and SS41, and also weidability of SS41 and SUS304 is better than SS41 and SM45C. Comparing mechanical properties with AE counts, it is found that AE conuts appeared on a small before the limit load of elasticity(P$_{e}$), and apper greatly near yield strength region in tension test. These results could contribute to the safety analyses and the evaluation of strength for welding structure.e.

• 한국융합학회논문지
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• 제8권7호
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• pp.231-236
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• 2017

본 연구에서는 고분자재료인 CFRP(Carbon Fiber Reinforced Plastic)과 구조용 금속인 SM45C로 이루어진 이종 복합재료가 경량화 재료용으로 사용되고 있다. SM45C를 심재로 갖고 양면에 섬유 적층각도가 다른 단반향 CFRP를 접착시킨 샌드위치형 복합재료를 이용하여 CT(Compact Tension)시험을 기초로 한 유한요소 해석을 진행하였다. CT시험은 하중을 받는 재료내의 크랙으로 인한 파괴거동을 확인하기 위한 대표적인 방법이다. 이종 복합재료를 기계 구조물에 적용하기 위해서는 크랙 및 구멍에 대한 영향을 연구하여야 한다. 샌드위치형 복합재료의 CT시험에 의한 파괴거동을 시뮬레이션 해석으로 연구하였다. 본 연구 결과로서, [0/60/-60/0]의 적층각도를 가진 단방향 CFRP 샌드위치형태 복합재료가 우수한 강도를 갖으며 최대 등가응력은 약 182GPa정도가 나타났다. 또한 복합 재료 형상으로서의 디자인적 요소를 융합 기술에 접목함으로서 그 미적인 감각을 나타낼 수 있다.

• 대한기계학회논문집A
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• 제28권8호
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• pp.1109-1115
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• 2004

The objective of this study is to elucidate what governs delayed hydride cracking (DHC) in Zr-2.5Nb tubes by correlating the striation spacings with DHCV(DHC Velocity). To this end, DHC tests were conducted on the compact tension specimens taken from the Zr-2.5Nb tubes at different temperatures ranging from 100 to $300^{\circ}C$ with a 3 to 6 data set at each test conditions. The compact tension specimens were electrolytically charged with 27 to 87 ppm H before DHC tests. After DHC tests, the striation spacings and DHCV were determined with the increasing the test temperature and yield strength. The striation spacing and DHCV increased as a function of yield $strength^2$ and the temperature. Since the plastic zone size ahead of the crack tip can be represented by ${\sim}(K_{IH}/{\sigma}_{Y})^2$, we conclude that the striation spacing is governed by the plastic zone size which in turn determines a gradient of hydrogen concentration at the crack tip. The relationship between the plastic zone size and the striation spacing was validated through a complimentary experiment using double cantilever beam specimens. Two main factors to govern DHCV of Zr-2.5Nb tubes are concluded to be hydrogen diffusion and a hydrogen concentration gradient at the crack tip that are controlled by temperature and yield strength, respectively. The activation energy of DHCV in the Zr-2.5Nb tubes is discussed on the basis of temperature dependency of hydrogen diffusion and the striation spacing.

• 한국항해항만학회지
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• 제26권4호
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• pp.435-440
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• 2002

잔류응력이 판의 파괴 특성에 미치는 영향의 정량적 평가를 위하여, 균열이 존재하는 CT(Compact Tension) 시편에 가스 토오치 (gas torch)를 이용한 국부 가열을 실시하여 인위적인 잔류응력을 생성시키고, 열탄소성 유한요소해석을 통하여 생성된 잔류응력장을 평가하였으며, 잔류응력이 존재하는 시편과 잔류응력이 존재하지 않는 시편에 대한 파괴인성 실험을 실시하여 이들의 결과를 파괴저항 선도 상에서 비교, 분석함으로써 압축 잔류응력이 파괴 특성에 미치는 영향을 정량화하였다.

• Corrosion Science and Technology
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• 제3권1호
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• pp.14-19
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• 2004

Crack growth rate and threshold stress intensity factor for stress corrosion cracking(SCC), $K_{ISCC}$ were measured for type 403 stainless steel in 3,5% NaCl solution at room temperature and SCC was monitored by electrochemical noise technique during $K_{ISCC}$ testing. In rising load test, pits were formed at the tip of pre-crack for the pre-cracked compact tension specimen unlike in smooth round specimen in which only unstable pits were observed and hence immune to SCC. Micro-cracks were found to initiate from the pits in the former specimen, and initiation of micro-crack as well as macro-crack was detected by electrochemical noise technique in rising load $K_{ISCC}$ tests. Crack growth rate increased with increasing either displacement rate or stress intensity factor at crack initiation and was higher in rising load $K_{ISCC}$ test compared to constant load $K_{ISCC}$ test at given stress intensities.