• Journal of Adhesion and Interface
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• v.15 no.4
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• pp.174-177
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• 2014

• Journal of Adhesion and Interface
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• v.5 no.2
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• pp.40-50
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• 2004

• Composites Research
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• v.24 no.2
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• pp.1-8
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• 2011

Interfacial fracture toughness under various mixed-mode loading is measured to provide a mixed-mode fracture criterion of a composite/metal bonded joint. Experimental fracture characterization tests were carried out using a SLB (single leg bending) specimen, which controls mode ratio with the specimen thickness. The experimental result of the SLB test conforms that interfacial fracture toughness increases as the mode II component increases. The effect of loading mode on interfacial crack growth is investigated on the basis of crack path observation using microscopic image acquisition technique. The influence of interfacial roughness on adhesion strength is also discussed.

• Adhesion and Coating Technology
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• v.1 no.1
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• pp.7-14
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• 2022

• Journal of Adhesion and Interface
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• v.5 no.1
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• pp.12-20
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• 2004

Interfacial fracture mechanics is introduced and its application to adhesion measurement is reviewed. Various specimens are also introduced for the practical application.

• Journal of the Korean Society of Propulsion Engineers
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• v.16 no.3
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• pp.9-15
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• 2012

This research simulates the ultrasonic wave propagation in multi-layered media using generalized formular of system response function. We made the artificial defect specimen of a rocket motor and compared with experimental wave forms. The simulation results are coincide with measured waves and we found that the pulse echo method is able to detect unbond defect at liner-propellant interface.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2011.11a
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• pp.912-918
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• 2011

This research simulates the ultrasonic wave propagation in multi-layered media using generalized formular of system response function. We made the artificial defect specimen of a rocket motor and compared with experimental wave forms. The simulation results are coinciede with mesuared waves and we found that the pulse echo method is able to detect disbond at liner-propellant interface.

• Journal of the Korean Applied Science and Technology
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• v.35 no.1
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• pp.141-150
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• 2018

Mussel byssal protein has strong adhesive capability even in wet surface. It has been reported that nine proteins in marine blue mussel, often referred to a representative mussel, contribute to form mussel byssal threads and plaques. DOPA containing two hydroxy groups called cathecol is recognized that it plays a major role in adhesion as well as cohesion process within byssal structure. In this paper, adhesion and cohesion mechanisms were introduced and evaluated by supportive literature published during last decade. Diverse applications of cathecol chemicals were also examined in terms of innovative adhesive, bioadhesive and challenging material for tissue engineering. It is noticeable that reconsideration of mussel proteins could provide the various opportunities as biomaterials.

• Composites Research
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• v.19 no.4
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• pp.15-22
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• 2006

One of the primary factors limiting the application of composite-metal adhesively bonded joints in structural design is the lack of a good evaluation tool for the interfacial strength to predict the load bearing capacity of boned joints. In this paper composite-steel adhesion strength is evaluated in terms of stress intensity factor and fracture toughness of the interface corner. The load bearing capacity of double lap joints, fabricated by co-cured bonding of composite-steel adherends has been determined using fracture mechanical analysis. Bi-material interface comer stress singularity and its order are presented. Finally stress intensities and fracture toughness of the wedge shape bi-material interface corner are determined. Double lap joint failure locus and its mixed mode crack propagation criterion on $K_1-K_{11}$ plane have been developed by tension tests with different bond lengths.

• Journal of the Korean Society of Propulsion Engineers
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• v.24 no.5
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• pp.84-90
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• 2020

The adhesion strength of two konds of solid propellants(primary propellant/secondary propellant) was studied by coating agent of adhesion composition composed of organic solvent, curing agent, and cure catalyst. The coating agent using FeAA, cure catalyst, resulted propellant breaking at more 0.14 wt% and interface breaking at less 0.10 wt%. The TPB cure catalyst of confirmed the result of the interface breaking immediately after curing of the secondary propellant. In addition, the coating agent using TPB was found to increase the adhesion strength between the primary propellant and the secondary propellant over time.