• Journal of the Computational Structural Engineering Institute of Korea
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• v.35 no.3
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• pp.191-196
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• 2022

In this study, the anisotropic mechanical property of fused deposition modeling three-dimensional (3D) printing based on lamination direction was verified by a tensile test. Moreover, the property was applied to solid isotropic materials with penalization-based topology optimization. The case of the lower control arm, one of the automotive suspension components, was considered as a benchmark problem. The optimal topological results varied depending on the external load and anisotropic property. Based on these results, two test specimens were fabricated by varying the lamination direction of 3D printing; a tensile test utilizing 3D non-contact strain gauge was also conducted. The measured strain was compared with that obtained by computer-aided engineering response analysis. Quantitatively, the measurement and analysis results are found to have good agreement. The effectiveness of topology optimization considering the lamination direction of 3D printing was confirmed by the experimental result.

• Proceedings of the Materials Research Society of Korea Conference
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• 2003.11a
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• pp.162-162
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• 2003

최근에 산화물 인공격자의 우수한 특성으로 인하여 활발한 연구가 진행되고 있다. 본 연구에서는 펄스레이저 증착방법을 이용하여 산소분압 100mTorr, $650^{\circ}C$에서 LSCO/MgO 기판위에 La-50mol% 첨가된 SrTiO$_3$ (SLTO)와 SrTiO$_3$ 를 적층시켜 산화물 인공격자를 만들어 결정구조에 대하여 연구하였다. SrTiO$_3$ (STO)는 상온에서 3.904$\AA$인 cubic perovskite 구조를 가지고 있다. 일반적으로 La$^{3+}$ (1.14$\AA$)은 Sr$^{2+}$(1.12$\AA$)과 이온반경이 거의 유사하기 때문에 ABO 페로브스카이트 구조의 A자리에 치환될 것으로 기대되며 또한 Sr$^{2+}$ 자리에 La$^{3+}$ 가 치환되므로써 발생하는 charge compensation은 Sr 자리에 Vacancy 생성으로 판단된다. 인공격자의 성장확인을 위하여 SLTO와 STO를 10층씩 증착하여 XRD분석을 통하여 평가하여 보았다. 확인된 결과를 바탕으로 산화물 인공격자의 적층 주기를 SLTO layer를 한층으로 고정시키고 STO를 한 층에서 다섯 층까지 다양하게 변화시켰다. 본 연구의 목적은 산화물 인공격자에서 결정결함을 제어하여 소자에 응용할 수 있는 전기적 물성을 평가하기 위함이다. X-ray diffraction 결과 SLTO/STO 인공격자는 (001) 방향으로 우선배향하였으며 적층주기에 따라 격자상수의 변화를 보였다. AES의 depth profile 분석을 통하여 La의 분포를 확인하였으며, HRTEM 분석을 통하여 미세구조분석을 실시하였다.

• Transactions of the Korean Society of Mechanical Engineers
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• v.10 no.6
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• pp.929-936
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• 1986

Free vibration characteristics of laminated orthotropic circular cylindrical shells with clamped free boundary condition are investigated. The solution is obtained through a direct solution procedure with axial mode displacements represented as simple Fourier series expressions. On the basis of the thin shell theories of Sanders, Love, Loo, Morley and Donnell, the 4*$ frequency determinant is derived and is expressed in a unified form. Various numerical examples determining the natural frequencies of circular cylindrical shells with isotropic material and also with layers of orthotropic elastic material arbitraily laminated either symmetrically or anti-symmetrically about the shell middle surface. The results obtained compared very well with some available experimental and numerical results.

• Proceedings of the Materials Research Society of Korea Conference
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• 2009.05a
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• pp.19.2-19.2
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• 2009

ITO는 n형 반도체 특성을 가지며 이와 동시에 높은 가시광투과율과 낮은 전기전도도를 가짐으로써 다양한 투명전극소재와 가스 검출센서로 많이 활용되고 있다. 본 연구에서는 RF magnetron sputtering 법을 이용하여 상온에서 glass 기판 위에 두께 100nm로 ITO 그리고 하층 ITO 박막 (두께 50 nm) 위에 층간 금속 (두께 5 nm)을 증착하고 다시 상부 ITO 박막 (두께 45 nm)을 증착하여 3층의 적층형 박막센서를 제작하였다. 층간 금속으로는 Au와 Cu를 각각 사용하였다. 박막 증착 후엔 진공분위기에서 $150^{\circ}C$, $300^{\circ}C$로 열처리 과정을 거쳐 열처리 전후의 물성 및 감지특성을 비교해보았다. 분석방법으로는 XRD, SEM, AFM, Hall effect 장치 등을 이용하였다. 분석 결과 $300^{\circ}C$에서 진공 열처리한 ITO/Au/ITO(IAI) 박막센서가 높은 결정화도 와 전기적 특성이 나타났으며, 0 에서 1000ppm 까지의 메탄가스의 민감도 측정에서도 열처리된 IAI 박막센서가 기존의 ITO 박막센서보다도 약 70% 정도 향상된 민감도를 나타내었다.

• Journal of the Korean Society of Manufacturing Process Engineers
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• v.20 no.8
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• pp.52-59
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• 2021

In this study, we experimentally evaluated the mechanical properties and geometric form accuracy in FDM 3D printing processes based on the printing direction, building direction, and layer thickness. The specimen test results showed that the tensile strength increased by over 33% in the printing direction compared to the direction perpendicular to printing and the tensile strength becomes larger as the layer thickness decreased. Furthermore, the tensile and impact strengths in the building direction were significantly reduced due to the difference in the interlayer joining and bonding strengths of the fused material. Additionally, shrinkage of the material due to phase change induced curl distortion especially in thin and long 3D-printed products, which increased as the layer thickness increased.

• Composites Research
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• v.23 no.6
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• pp.61-66
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• 2010

In this paper, the variation of mechanical properties of T800 carbon/epoxy composites according to the forming pressure, which was referred to previous studies on a filament winding process, were investigated. The specimens of all the tests were fabricated by an autoclave de-gassing molding process controlling forming pressure (absolute pressures of 0.1MPa, 0.3MPa, 0.7MPa including vacuum) and water jet cutting after fabricating composite laminates. Various tensile tests were performed for in-plane properties and interlaminar properties were also measured by using Iosipescu test jig. Fiber volume fraction was measured to correlate the property variation and the forming pressure. This properties are expected to be utilized in the design of Type III pressure vessel for hydrogen vehicles which uses the same carbon fiber (T800 carbon fiber) for the filament winding process.

• Composites Research
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• v.32 no.5
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• pp.229-236
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• 2019

In this study, the effects of the additional processing parameters on the mechanical properties of thermoplastic composites fabricated with automated fiber placement (AFP) were evaluated. Annealing and vacuum bag only processes were then performed on the manufactured thermoplastic composites, respectively. For verification, the crystallinity was measured by differential scanning calorimetry (DSC), confirming the variation of semi-crystalline thermoplastic composite according to the process conditions. The void content of thermoplastic composites was evaluated by matrix digestion method while microscopic examination confirmed the porosity distribution. The interlaminar shear strength test was conducted for three different process parameters (VBO, annealing, and no treatment). A comparison of the three tested strengths was made, revealing that the porosity value had larger effect on the mechanical properties of the thermoplastic composite compared to the degree of crystallinity. Additionally, when thermoplastic composite melted up, the pores were continuously removed under vacuum process; the removal of the pores resulted in an increase of the interlaminar shear strength.

• Proceedings of the Korean Society For Composite Materials Conference
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• 2005.04a
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• pp.221-225
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• 2005

성층권 비행선 기낭용 막재료를 개발하였다. 성층권 비행선을 구현하기 위한 초경량/고강도의 막재료를 설계 개발하였다. 요구조건을 만족시키기 위하여 벡트란, 테들라 등의 최신 고분자 화합물을 적층한 막재를 개발하였다. 개발된 막재료에 대한 유한요소 미세구조 모델링을 수행하고, 물성치를 예측하였다. 막재료에 대한 물성시험을 수행하였다. 단위 시편에 대한 강도-강성 시험을 수행하였으며, 이를 유한요소 예측치와 비교하였다.

• Journal of the Korean Society for Precision Engineering
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• v.29 no.9
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• pp.938-945
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• 2012

To design and estimate material failures of Type III pressure vessels, which have excellent stability and performance, various modeling techniques have been introduced. This paper provided a hybrid modeling technique composed of ply-based modeling for a cylinder part and laminate-base modeling technique for a dome part for enhancing modeling efficiency. The ply-based modeling technique provided accurate ply stresses directly for predicting material failure, on the other hand, additional manipulations in stress calculations, which may cause some errors, were needed for the case of the laminate-based modeling technique. The ply stresses in fiber, transverse and in-plane shear directions were compared with the corresponding material strengths to predict material failure.

• Composites Research
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• v.16 no.6
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• pp.41-47
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• 2003

Composites are widely used for aircraft, satellite and other structures due to its good mechanical and thermal characteristics such as low coefficient of thermal expansion(CTE), heat-resistance, high specific stiffness and specific strength. In order to use composites under condition of high temperature, however, material properties of composites at high temperatures must be measured and verified. In this paper, material properties of T700/Epoxy were measured through tension tests of composite specimens with an embedded FBG sensor in the thermal chamber at the temperatures of RT, $100^{\circ}$, $200^{\circ}$, $300^{\circ}$, $300^{\circ}$. Through the pre-test of an embedded optical fiber, we confirmed the embedding effects of an optical fiber on material properties of the composites. Two kinds of specimens of which stacking sequences are [0/｛0｝/0]$_{T}$. and [$90_2$/｛0｝/$90_2$]. were fabricated. From the experimental results, material property changes of composites were successfully shown according to temperatures and we confirmed that fiber Bragg grating sensor is very appropriate to strain measurement of composites under high temperature.