• 터널과지하공간
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• 제7권2호
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• pp.108-115
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• 1997

Uniaxial and biaxial compressive tests were conducted on limestone specimens containing artificial joints and a circular hole to investigate the influence of inclination and number of joints on compressive strength and deformation behavior of rock with a circular hole. Under uniaxial and biaxial compressive condition, the inclination of joints showing the maximum and minimum strength were 0$^{\circ}$ and 30$^{\circ}$ respectively, which was independent of the number of joints. Under uniaxial compressive condition, relative maximum strength of rock with n=1 and 3 to intact rock with a circular hole were 12.5%~82.8% and 11.4~62.5% respectively, and under biaxial compressive condition, 18.2~91.0% and 17.0~87.5% respectively. The influence of the number of joints on the decrease of compressive strength was greater under uniaxial than under biaxial compressive condition. Under uniaxial and biaxial compressive condition, axial and lateral deformations of rock showed the least values where $\alpha$=30$^{\circ}$. Under uniaxial compressive condition, axial and lateral deformation at maximum strength of rock have the increasing tendency with increase the number of joints. But they have the decreasing tendency under biaxial compressive condition. Under uniaxial and biaxial compressive conditions, axial deformation of circular hole was greater than lateral deformation without respect to the number of joints and the inclination of joints.

• Structural Engineering and Mechanics
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• 제38권3호
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• pp.361-384
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• 2011

Earlier studies on hollow-circular rubber bearings, all of which are conducted for steel-reinforced bearings, indicate that the hole presence not only decreases the compression modulus of the bearing but also increases the maximum shear strain developing in the bearing due to compression, both of which are basic design parameters also for fiber-reinforced rubber bearings. This paper presents analytical solutions to the compression problem of hollow-circular fiber-reinforced rubber bearings. The problem is handled using the most-recent formulation of the "pressure method". The analytical solutions are, then, used to investigate the effects of reinforcement flexibility and hole presence on bearing's compression modulus and maximum shear strain in the bearing in view of four key parameters: (i) reinforcement extensibility, (ii) hole size, (iii) bearing's shape factor and (iv) rubber compressibility. It is shown that the compression stiffness of a hollow-circular fiber-reinforced bearing may decrease considerably as reinforcement flexibility and/or hole size increases particularly if the shape factor of the bearing is high and rubber compressibility is not negligible. Numerical studies also show that the existence of even a very small hole can increase the maximum shear strain in the bearing significantly, which has to be considered in the design of such annular bearings.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 1997년도 추계학술대회 논문집
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• pp.731-734
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• 1997

In this study, a shape optimization is performed for circular and elliptical holes to reduce weight of a plate. It is accomplished in reference to the results of topology optimization of the square plate with circular hole. From the results. it is concluded that the stress values of shape optimization of them are satisfied with 100MPa of constraint condition.

• Steel and Composite Structures
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• 제2권4호
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• pp.237-246
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• 2002

In this paper, the solution of a semi-infinite plane with one circular hole is presented. This solution is induced by repeatedly superposing the solution of an infinite plane with one circular hole and that of a semi-infinite plane without holes to cancel out the stresses arising on both boundaries. This procedure is carried out until the stresses arising on both boundaries converge. This method does not require complicated calculation procedures as does the method using stress functions defined in a bipolar coordinate system. Some numerical results are shown by graphical representations.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 추계학술대회논문집A
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• pp.278-285
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• 2001

Aluminum/Aramid Fiber Reinforced Plastic(Al/AFRP) laminates are applied to the fuselage-wing intersection. The main objective of this study was to evaluate the delamination zone behavior of Al/AFRP with a saw-cut and circular hole using average stress criterion and the effect of notch geometry. Mechanical tests were carried out to determine the cyclic-bending moment and delamination zone observed ultrasonic C-scan pictures. In case of Al/AFRP containing saw-cut specimen, the shape and size of the delamination zone formed along the fatigue crack. However, in case of Al/AFRP containing circular hole specimen, the shape and size of delamination zone formed two types. first type, delamination zone formed along the fatigue crack. Second type, not observed fatigue crack. Therefore, delamination zone was formed dependently of the circular hole shape.

• Journal of Advanced Marine Engineering and Technology
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• 제32권6호
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• pp.834-840
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• 2008

We carried out fatigue testing with materials of aluminum alloyC7075-T6, 2024-T4) by rotary bending fatigue tester. We investigated fatigue limit, fatigue crack initiation, fatigue crack propagation behavior and possibility of fatigue life prediction to the different small circular hole defect. The summarized result are as follows; Fatigue limit of the smooth specimens were related tensile strength and yield strength. In case of more large applied stress and small circular hole crack defect, the fatigue crack was grown rapidly. The fatigue crack propagation behavior proceed at according to inclusion. Fatigue crack propagation ratio appeared instability and retardation phenomenon in the first half of fatigue life but appeared stability and replied in the latter half. On other hand, this experimental data of the materials are appeared fatigue life predictability.

• 수산해양기술연구
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• 제19권1호
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• pp.51-56
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• 1983

경계요소법에 의하여 U자형 홈(groove)을 가진 평판이 측면 분포하중을 받을 때 끝부에 위치할 원형 Hole의 최적 위치의 해석을 행하고 동일한 모델(model)에 대하여 실험결과를 비교하여 다음과 같은 결론을 얻게 되었다. 1. 원형 Hole이 U자형 홈(groove)에 가까이 접근하게 됨에 따라 초기의 원형 Hole은 c.-c.선에 수직방향이 그 장축이 되는 타원형으로 변화됨을 알 수 있다. 2. 원형 Hole이 U-groove에 접근함에 따라 Hole 과 Groove 사이의 Neck부는 그 횡단면응력이 인장 및 압축이 동시에 존재하다가 점점 전체가 인장역이 됨을 알 수 있다. 3. 원형 Hole이 Groove에 접근함에 따라 판재경계와 Hole 사이의 목(neck)부분은 계속적인 압축상태를 유지한다. 4. U-groove쪽의 Neck area의 응력분포는 그 최대응력치가 Hole로 접근함에 따라 가속적으로 증가하고 Hole의 찌그러짐(distortion)의 방지를 위한 Hole의 최적중심의 위치는 Neck부의 Hole 측면의 압축응력치가 0이 되지 않는 범위가 한계임을 알 수 있다.

• 한국항공우주학회지
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• 제36권10호
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• pp.954-961
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• 2008

원형 손상구멍이 있는 날개 주위 유동장에 대한 실험연구를 수행하였다. 손상은 시위의 10% 직경의 시위에 수직인 원형 구멍으로, 구멍 중심은 1/4 시위 혹은 1/2 시위에 위치하고 있다. 입자영상유속계에 의한 유동장 측정과 날개의 아래 및 윗면에서의 정압장을 시위를 기준으로 한 레이놀즈수 Rec=2.85×105에서 측정하였다. 입자영상유속계에 의한 유동 측정 결과 손상 구멍 주위에는 두 가지 형태의 유동구조가 형성되었다. 하나는 약한 제트로 손상 구멍 하류에서 부착된 후류가 생성된다. 다른 하나는 받음각 증가에 의한 강한제트에 의한 것으로 손상구멍으로부터 자유흐름으로 관통되어 접근하는 경계층 흐름을 박리시켜 역류가 있는 박리 후류구조를 생성한다. 날개면 압력 자료는 원형 손상 구멍 근처에서 큰 압력변화를 보여주었다. 이러한 압력변화는 손상구멍이 앞전 쪽에 가까울수록 증가하였다.

• 대한기계학회논문집A
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• 제31권3호
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• pp.344-354
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• 2007

The objective of this study is to investigate the effect of arbitrarily located defect around the circular hole in the aircraft structural material such as Al/GFRP laminates and monolithic Al alloy sheet under cyclic bending moment. The fatigue behavior of these materials may be different due to the defect location. Material flaws in the from of pre-existing defects can severely affect the fatigue crack initiation and propagation behavior. The aim of this study is to evaluate effects of relative location of defects around the circular hole in monolithic Al alloy and Al/GFRP laminates under cyclic bending moment. The fatigue behavior i.e., the stress concentration factor($K_t$), the crack initiation life($N_i$), the relationship between crack length(a) and cycles(N), the relationship between crack growth rate(da/dN) and stress intensity factor range(${\Dalta}K$) near a circular hole are considered. Especially, the defects location at ${\theta}_1=0^{\circ}\;and\;{\theta}_2=30^{\circ}$ was strongly effective in stress concentration factor($K_t$) and crack initiation life($N_i$). The test results indicated the features of different fatigue crack propagation behavior and the different growing delamination shape according to each location of defect around the circular hole in Al/GFRP laminates.

• 비파괴검사학회지
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• 제19권3호
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• pp.173-179
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• 1999

고주파를 이용하여 금속 표면의 원형 프레스 결함, 원형 관통 결함 및 선형 프레스 결함 등을 조사하였다. 본 실험에서는 3kHz 변조된 9.2GHz의 주파수를 사용했으며, 조사 방법으로는 반사법, 투과법, 주파수 고정법 등을 이용하였다. 고주파가 원형 프레스 결함과 원형 관통 결함에서 반사 신호의 크기가 큰 폭으로 변했다. 원형 프레스 결함에서는 반사신호에 의한 결함의 크기가 원래 크기의 2.5배로 확대되어 측정되었으며, 원형 관통 결함에서는 결함의 크기가 두 배로 확대되어 측정되었다. 또한, 선형 결함에서 고주파 반사신호의 크기는 결함폭의 증가와 함께 커졌으며, 결함 깊이가 2.4mm일 때 결함폭이 50mm에서, 결함 깊이가 1.2mm 및 0.45mm에서는 결함폭이 55mm일 때 각각 최대값을 나타냈다.