• 대한기계학회논문집
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• 제13권1호
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• pp.87-95
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• 1989

본 연구에서는 국내산 비규칙성 짧은 섬유로 강회된 SMC 복합재료의 피로파괴 특성에 대한 기초자료로서 피로균열의 진전특성을 나타내는데 기존파괴 역학의 적용여부를 살펴보며, 서로 다른 피로모드 상태 하에서 하중크기의 상태에 따른 피로균열진전의 특성을 나타내었으며, 또한 주사형 전자현미경(scanning electron microscope)을 사용한 파단면 관찰을 통해 파괴 메카니즘을 살펴보았다.

• 대한기계학회논문집A
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• 제27권4호
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• pp.623-631
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• 2003

It is considered that the application of advanced composite materials to the prostheses for the disables is important to improve their bio-mechanical performance. Particularly, energy storing foot prosthesis is mostly important to restore gait ability of the disables with low-extremity amputation since it could provide propulsion at terminal stance enhancing the disables ability to walk long distance even run and jump. Therefore, the energy storing spring of Prosthetic foot keel under cyclic bending moment use mainly of high strength glass fiber reinforced plastic. The main objective of this study was to evaluate the stacking sequence effect using the delamination growth rate(dA$_{D}$/dN) of energy storing spring in glass fiber reinforced plastic under cyclic bending moment. The test results indicated that the shape of delamination zone depends on stacking sequence in GFRP laminates. Delamination area(A$_{D}$) turns out that variable types with the contour increased non-linearly toward the damage zones.nes.

• Journal of Welding and Joining
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• 제7권1호
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• pp.42-50
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• 1989

The application of fracture mechanics is being increased gradually to assess the safety of welded structures containing crack. Fatigue crack propagation behavior and elastic-plastic fracture toughness J$_{IC}$ of home made flux cored wire(1.22mm) CO$_{2}$ weldments was discussed. Especially fatigue crack propagation test was carried out by .DELTA.K control instead of load control and elastic-plastic fracture toughness J$_{IC}$ was obtained by ASTM-R curve method on C.T.specimen in transverse direction of weldments. The results obtained are as follows; (1) Weld metal presented an almost complete similarity to base metal on fatigue crack propagation rate in transverse direction. (2) Weld metal was more than base metal on J$_{IC}$ value in transverse direction. (3) F.C.W. CO$_{2}$ weldments had an excellent characteristic of fatigue crack propagation rate and J$_{IC}$ in less than 50kg/mm$^{2}$ steel grade, this would result from that weld metal had good static strength.trength.

• 대한기계학회논문집
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• 제16권9호
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• pp.1605-1614
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• 1992

본 연구에서는 고장력 7075-T73 알루미늄합금에 대하여 변동하중의 기보파형 인 단일과대하중과 고-저(high-low) 블럭하중하의 지연거동에 미치는 과대하중비 %O.L., 기준응력확대계수범위 .DELTA. $K_{b}$ 및 무차원 균열깊이 a/W의 영향을 규명하였 으며, 또한 Wheeler모델의 수정에 의한 예측피로수명을 실험치와 함께 검토하였다.다.

• 대한기계학회논문집A
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• 제21권10호
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• pp.1674-1682
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• 1997

Fatigue tests were performed to investigate the effect of ceramic coatings as in TiN and TiCN on fatigue crack growth properties of ceramic coated 1Cr-1Mo-0.25V steel with different coating thickness in laboratory air conditions. The experimental results are described with respect to a Paris equation, da/dN=C(.DELTA.K)$^{m}$ , where the crack growth rate of coated specimens provided as similar growth rate as that of the uncoated specimen regardless of coating thickness. Furthermore, it was observed that the type of coating layer had virtually no effect on crack growth rate in the full region of stress intensity factor range. And it was also appeared that the final crack length of TiCN coated specimens was short compared to that of TiN coated, and the substrate specimens, in which it was inferred due to lowering the toughness of coated material from high hardness of TiCN coating layer itself.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 추계학술대회논문집A
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• pp.231-237
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• 2000

A15052/AFRP laminates were developed principally to obtain a material with good fatigue strength, in which possible cracks would grow very slowly. Weight savings of more than 30% should be attainable in practice. Also, the crack bridging fibers could still was carry a significant part of the load over the crack, thus the COD and stress intensity factor was reduced at the crack tip. A15052/ AFRP laminates consists of three thin sheets of 5052-H34 aluminum alloy and two layers of [0] unidirectional aramid fiber prepreg. The cyclic-bending moment test was investigated based on applying the five kinds of bending moments. The size of the delamination zone produced between 5052-H34 aluminum alloy sheets and fiber-adhesive layers was measured from ultrasonic C-scan pictures taken around the fatigue crack. In addition, the relationship between the cyclic-bending moment and the delamination zone size was studied and the effect of fiber bridging mechanism was also considered.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 추계학술대회
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• pp.1062-1067
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• 2003

In this study, corrosion fatigue characteristics of CF8M and CF8A steel were investigated on the simulated PWR condition(Temp.:$316^{\circ}C$, Pres.: 15:MPa). To make the simulated PWR condition. the special test machine consisted of INSTRON, Autoclave, LOOP and Measurement system was developed. As ${\Delta}K$ is ranged from 11 to $20MPa{\sqrt{m}}$, Crack growth rate of PWR condition is faster than air condition. Above $20MPa{\sqrt{m}}$, the crack growth rate of PWR and air condition is similar. Corrosion fatigue characteristics regardless of the ferrite contents($10{\sim}25wt.%$) is not different. After the test, the fracture surface of specimens was examined. It was difficult to verify the fracture modes such as striation, intergranular crack and cleavage and so on. As the ferrite content of CF8M is increased, the more particles covered fracture surface were peeled.

• 대한기계학회논문집A
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• 제28권3호
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• pp.281-288
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• 2004

The hybrid composite material (Al/GFRP laminates) are applied to the fuselage and wing in a aircraft. Therefore, Al/GFRP laminates suffer from the cyclic bending moments. This study was to evaluate the effect of fiber stacking angle on the fatigue crack propagation and delamination behavior using the relationship between crack growth rate (da/dN) and stress intensity factor range (ΔK) in Al/GFRP laminates under cyclic bending moment. The variable delamination growth behavior in case of three different type of fiber orientations, i.e., [Al/O$_2$/Al], [Al/+45$_2$/Al] and [Al/90$_2$/Al] at the interface of Al layer and glass fiber layer was measured by ultrasonic C-scan images. As results of this study, It represent that the delamination shape should turns out to have more effective characteristics on the fiber stacking angle. The extension of the delamination zone in case of [Al/+45$_2$/Al] and [Al/90$_2$/Al] were not formed along the fatigue crack profile. The shape of delamination zone depend on fiber stacking angle and the variable type with the delamination contour decreased non-linearly toward the crack tip at the Al layer.

• 대한기계학회논문집A
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• 제28권2호
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• pp.174-180
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• 2004

If Fiber Reinforced Metal Laminates(FRMLs) were delaminated, the decrease of stiffness and fiber bridging effect would result in the sudden aggravation of fatigue characteristics. It was reported that the delamination of FRMLs resulted from the crack of metal layers and that it depended on the crack growth. While cracks were made in FRMLs containing a saw-cuts under fatigue loading, cracks could be produced or not in FRMLs with circular holes under the same condition. When the FRMLs with the circular holes produce not the crack but the delamination, it is not possible to analyze it by the conventional fracture parameters expressed as the function of the crack. And so, this research suggests a new analytical model of the delamination to make the comparison of the delamination behavior possible whenever the cracks occur or not. Therefore, a new analytical model called Pseudo Crack Model(PCM) was suggested to compare the delaminations whether cracks were made or not. The relationship between the crack energy consumption rate( $E_{crack}$) and the delamination energy consumption rate( $E_{del}$) was discussed and it was also known that the effect of $E_{del}$ was larger than that of $E_{crack}$.

• 대한토목학회논문집
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• 제4권2호
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• pp.133-142
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• 1984

횡방향(橫方向)과 종방향(縱方向), 대입열용접(大入熱鎔接)과 소입열용접(小入熱鎔接), 모재(母材)와 같은 강도(强度)의 용접재료(鎔接材料) 사용(使用)과 모재(母材)보다 낮은 강도(强度)의 용접재료(鎔接材料) 사용(使用) 등으로 서로 비교되는 용접(鎔接)이음의 소인장시험편(小引張試驗片)을 만들어서 피로시험(疲勞試驗)을 행하여 피로구열(疲勞龜裂) 진전속도(進展速度) ${\frac{da}{dN}}$와 구열선단(龜裂先端) 부근의 응력확대계수(應力擴大係數)의 변동범위(變動範圍) ${\Delta}K$와의 관계곡선(關係曲線)을 그려서 비교시험간(比較試驗間)의 모재(母材), 열영향부(熱影響部) 및 용착금속부(鎔着金屬部)로 구분, 혹은 지금까지의 연구자료(硏究資料) 등과 비교검토하였다. 이 결과, 다음과 같은 현상들을 알 수 있었다. 기본적(基本的)으로, 용접방향(鎔接方向), 용접입열량(鎔接入熱量), 용접재료(鎔接材料)의 강도(强度), 혹은 모재(母材), 열영향부(熱影響部) 및 용착금속부(鎔着金屬部)의 구분 등에 따라 ${\frac{da}{dN}}-{\Delta}K$관계에 큰 차이가 없었다. 다만, 첫째, 소재(素材)에 대한 경우에 비해 대개 처음은 같은 ${\Delta}K$에서 ${\frac{da}{dN}}$가 상당히 늦다가 점차 증가하여 중간쯤에서 같아진 후 끝 부분에서 같은 ${\Delta}K$에서${\frac{da}{dN}}$가 다소 빨라짐을 알 수 있었다. 둘째, 열영향부(熱影響部)에서 용접금속부(鎔接金屬部)로 진전(進展)하면서 ${\frac{da}{dN}}$가 다소 늦어지는 것을 알 수 있었다. 셋째, 용접방향(鎔接方向)과 구열방향(龜裂方向)이 평행인 경우가 직각인 경우에 비해, 모재(母材)와 같은 용접재료(鎔接材料)를 쓴 경우 소입열용접(小入熱鎔接)인 경우가 대입열용접(大入熱鎔接)인 경우에 비해, 모재(母材)보다 낮은 용접재료(鎔接材料)를 쓴 경우 대입열용접(大入熱鎔接)인 경우가 소입열용접(小入熱鎔接)인 경우에 비해, 대입열(大入熱)의 평행용접(鎔接)의 경우를 제외한 모든 용접(鎔接)에서 모재(母材)와 같은 강도(强度)의 용접재료(鎔接材料)를 쓴 경우가 모재(母材)보다 낮은 강도(强度)의 용접재료(鎔接材料)를 쓴 경우에 비해 ${\Delta}K$가 낮은 시기(時期)에 일찍 저속(低速)으로 구열(龜裂)이 시작되어 ${\Delta}K$의 큰 증가없이 ${\frac{da}{dN}}$가 빠르게 증가한 다음 다른 경우와 같은 성상(性狀)으로 진전됨을 알 수 있었다. 넷째, 소입열용접(小入熱鎔接)의 경우 평행용접(鎔接)이 직각용접(鎔接)에 비해, 소입열용접(小入熱鎔接)이 대입열용접(大入熱鎔接)에 비해 같은 ${\Delta}K$에서 ${\frac{da}{dN}}$가 다소 늦은 것을 알 수 있었다.