• Transactions of the Korean Society of Mechanical Engineers
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• v.14 no.1
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• pp.23-36
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• 1990

The various composite materials have been developed with the development of high strength material and the increasement of composite material usage. Therefore many researchers have studied about the stress analysis and the fracture mechanics for composite materials through the experiment or the theory. Among the experimental methods, the photoelastic experiments have been used for the stress analysis of the isotropic structures or the anisotropic structures. To analyze the stresses in the orthotropic material with photoelastic experiment, the basic physical properties ( $E_{L}$, $E_{T}$, $G_{LT}$ , .nu.$_{LT}$ ) and the basic stress fringe values ( $f_{L}$, $f_{T}$, $f_{LT}$ )are needed, therefore the relationships between the basic physical properties and the stress fringe values were derived in this paper. When the stress fringe value is very large, it was assured by the experiment that the relationships are established both in the room temperature and in the high temperature (T = 130.deg. C). Therefore the basic physical properties can be obtained from the relationships by measuring stress fringe values instead of measuring the basic physical properties.rties.

• Transactions of the Korean Society of Mechanical Engineers
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• v.19 no.8
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• pp.1810-1821
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• 1995

Photoelastic experiment has been used to analyze stress of structure and stress in the vicinity of crack tip etc.. Model experiment such as photoelastic experiment has been restricted by problem of residual stress in the photoelastic model material. They are generated by molding, cutting and time effects etc.. They produce some errors in the results of photoelastic experiment data. In this paper, stress optic law considering residual stress already developed by authors was applied to the stress concentration problem and fracture mechanics. Although the specimen was bad with residual stress, we could obtain good results by using the stress optic law considering residual stress. It was found that the stress optic law of photoelastic experiment could be applied to the stress analysis of bimaterial.

• Journal of the KSME
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• v.31 no.3
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• pp.276-292
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• 1991

복합체 구조물을 광탄성 실험법으로 응력해석 하고자 할 때는 반드시 아래의 사항이 연구되어야 한다. (1) 복합체 구조물의 이방성 성질과 상사되는 광탄성 재료가 개발되어야 한다. (2) 광탄성 재료의 기본 물성치($E_L,E_r,G_{LT},V_{LT}$)와 응력 프린지치($f_L,f_r,f_{LT}$) 등이 측정되어야 한다. (3) 복합체 구조물의 응력 해석을 할 수 있는 광탄성 실험의 실험 방법이 개 발되어야 한다. 이론적으로 규명하기 힘들고 역학적으로 논란되고 있거나 인명에 관계되는 기 계나 구조물 등을 이론적으로 해결하였으나 실험적으로 확인하려고 할 때 광탄성 실험법은 확인 실험법으로써 매우 유용한 방법이므로 아래와 같이 요구된다. 광탄성 실험법이 앞에서 나열된 것처럼 파괴 역학의 여러 분야에도 유용하게 이용될 뿐만 아니라 의학 분야에도 매우 유용하게 이용되고 있다.

• Journal of the KSME
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• v.32 no.6
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• pp.536-553
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• 1992

하중 종류 중에서 가장 기본적인 하중 중의 하나인 순수 전단력과 순수 굽힘 모멘트를 발생시 키고자 할 때는 아래와 같은 장치를 사용하는 것이 좋다. 1) 등방성체나 이방성체의 횡 전단계수 (G$_{12}$)와 횡 응력 프린지치(f$_{12}$) 등을 측정 하고자 할 때, 또는 모드 II (mode II)상태의 파괴역학을 연구하고자 할 때는 그림 1, 그림 2, 그림 3 그리고 그림 4 등에 제시된 것 중에서 적당한 것을 사용할 수 있다. 그러나 순수 전단 력이 발생되는 면적이 크고, 순수 전단력을 정확하고 균일하게 발생시키고자 할 때, 각 재료의 전단 물성치(shear properties) 측정, 모드II(mode II) 상태의 파괴역학을 연구하고자 할 때는 본 연구자가 고안한 H.I.S.T. 장치를 이용하면 편리하다. 2) 직선 보에 순수 굽힘 모멘트를 균일하고 정확하게 가하고자 할 대는 N.B.M.장치를 사용하는 것이 좋다. 또 N.B.M. 장치는 어느 보의 장치보다도 곡선보나 변형이 큰 보에도 더 정확하고 균일하게 순수 굽힘 모멘트를 발생시킬 수 있다.

• Transactions of the Korean Society of Mechanical Engineers
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• v.19 no.8
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• pp.1876-1888
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• 1995

In this paper, glass surface-mat reinforced epoxy(G.S.R.E.) is developed, It is assured that the material(G.S.R.E.) can be used as photoelastic model material and it satisfy with the required properties of photoelastic model material. Therefore, the material can be used as model material of transparent photoelastic experiment when we analyze the stress distributions of transversely isotropic material by photoelastic experiment. When we use G.S.R.E. as photoelastic experiment model material, we had better use the G.S.R.E. which fiber volume ratio is less than 0.7% in the high temperature(stress freezing method) and than 1.74% in the room temperature. Relationships between stress fringe value and elastic modulus in transversely isotropic material are developed in this paper, it is assured by experiment that they are established in the room temperature or in the high temperature. Therefore we can obtain stress fringe value or elastic modulus from the relationships between stress fringe value and elastic modulus.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.22 no.3
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• pp.624-634
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• 1998

The photoelastic model material with shape memory effect and the molding processes for the material are developed in this research. The matrix and fiber of the photoelastic model material developed in this research are epoxy resin (Araldite to hardner 10 to 3 (weight ratio)) and wire of $Ti_50-Ni_50$ shape memory alloy, respectively. It is called Ti50-Ni50 Shape Memory Alloy Fiber Epoxy Composite $(Ti_50-Ni_50SMA-FEC).$ Ti50-Ni50 SMA-FEC is satisfied with the requirements of the photoelastic model material and can be used as a photoelastic model material. The maximum recovering strain of $Ti_50-Ni_50$SMA-FEC is occurred at $80^{\circ}C$ in any prestrain of $Ti_50-Ni_50$ shape memory alloy fiber and in any fiber volume ratio. Recovering strain(force) is increased with the increment of the prestrain and the fiber volume ratio. The best prestrain of $Ti_50-Ni_50$SMA-FEC is 5% for the recovering force among 1%, 3%, 5%.