• Composites Research
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• 제15권1호
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• pp.53-60
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• 2002

본 연구에서는 내열 특성과 구조적인 특성을 갖는 탄소섬유/페놀릭 복합재 내열튜브를 필라멘트와인딩 공법에 의해 제작하고 이들의 구조적인 성능을 평가하였다. 이를 위해 내열튜브의 제작방법을 소개하고 황산용해법을 적용하여 내열튜브에서의 섬유체적비와 기공함유율을 측정하였다. 시편폭을 달리한 인장시편의 기계적 특성을 평가함으로써 강화섬유의 연속성을 나타낼 수 있는 시편형상을 제시하였으며 공정변수를 달리한 내열튜브에서 채취된 인장시편의 기계적 특성을 평가함으로써 내열튜브의 제작을 위한 적절한 공정조건을 결정하였다. 그리고 보증시험을 통해 수집한 음향신호의 분석을 통해 내열튜브에서의 균열진전과 파손양상을 조사하였다. 마지막으로 내열튜브 자체에 대해 보증시험과 파열시험을 수행함으로써 내열튜브 자체의 구조적인 신뢰성을 확인하였다.

• Korean Journal of Radiology
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• 제19권6호
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• pp.1053-1065
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• 2018

Objective: To evaluate the clinical impact of using registration software for ablative margin assessment on pre-radiofrequency ablation (RFA) magnetic resonance imaging (MRI) and post-RFA computed tomography (CT) compared with the conventional side-by-side MR-CT visual comparison. Materials and Methods: In this Institutional Review Board-approved prospective study, 68 patients with 88 hepatocellulcar carcinomas (HCCs) who had undergone pre-RFA MRI were enrolled. Informed consent was obtained from all patients. Pre-RFA MRI and post-RFA CT images were analyzed to evaluate the presence of a sufficient safety margin (${\geq}3mm$) in two separate sessions using either side-by-side visual comparison or non-rigid registration software. Patients with an insufficient ablative margin on either one or both methods underwent additional treatment depending on the technical feasibility and patient's condition. Then, ablative margins were re-assessed using both methods. Local tumor progression (LTP) rates were compared between the sufficient and insufficient margin groups in each method. Results: The two methods showed 14.8% (13/88) discordance in estimating sufficient ablative margins. On registration software-assisted inspection, patients with insufficient ablative margins showed a significantly higher 5-year LTP rate than those with sufficient ablative margins (66.7% vs. 27.0%, p = 0.004). However, classification by visual inspection alone did not reveal a significant difference in 5-year LTP between the two groups (28.6% vs. 30.5%, p = 0.79). Conclusion: Registration software provided better ablative margin assessment than did visual inspection in patients with HCCs who had undergone pre-RFA MRI and post-RFA CT for prediction of LTP after RFA and may provide more precise risk stratification of those who are treated with RFA.

• Carbon letters
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• 제2권3_4호
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• pp.192-201
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• 2001

The Carbon/Carbon composite was prepared from 3D carbon fiber preform and coal tar pitch as matrix precursor. In order to evaluate of ablative characteristics of the composite, liquid rocket system was employed Kerosene and liquid oxygen was used as propellants, operating at a nominal chamber pressure of 330 psi and a nominal mixture ratio (O/F) of 2.0. The results of an experimental evaluation were that high density composite exhibited high, while low density composites showed low erosion resistance. The erosion rate against heat flux was highly depended on the density of the materials. The morphology of eroded fiber showed differently according to collision angle with heat flux on the composite. The granular matrix which derived from carbonization pressure of 900 bar was more resistance to heat flux than well-developed flow type matrix.

• 한국항공우주학회지
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• 제43권12호
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• pp.1048-1053
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• 2015

고온 환경에 노출되는 열 보호 시스템의 삭마 현상에 의한 표면 침식은 주로 재료의 두께 방향으로 진행된다. 본 논문에서는 0.4MW 아크 가열 풍동을 통한 삭마 실험을 수행하고 삼차원 표면 측정기를 이용하여 삭마 재료의 표면 상태를 측정하였다. 특히, 정밀한 삼차원 이미지 데이터를 획득하여 고온 플라즈마 환경에서 진행된 삭마 재료의 표면 거칠기와 침식량을 산출하였다. 이와 같은 삭마 실험 전후에 발생된 시편의 질량 감소도 함께 측정함으로써 표면 특성의 변화를 정량적으로 비교 및 분석하였다.

• International Journal of Aeronautical and Space Sciences
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• 제17권2호
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• pp.175-183
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• 2016

A poroelastic composite material, containing different material phases and filled with fluids, serves as a model to formulate the overall ablative behaviors of such materials. This article deals with the assessment of variation in nondeterministic poroelastic properties of two-phase composite materials using micromechanical representative volume element (RVE) models. Considering the configuration and arrangement of pores in a matrix phase, various RVEs are modeled and analyzed according to their porosity. In order to quantitatively investigate the effects of microstructure, changes in effective elastic moduli and poroelastic parameters are measured via finite element (FE) analysis. The poroelastic parameters are calculated from the effective elastic moduli and the pore-pressure-induced strains. The reliability of the numerical results is verified through image-based FE models with the actual shape of pores in carbon-phenolic ablative materials. Additionally, the variation of strain energy density is measured, which can possibly be used to evaluate microstress concentrations.

• Korean Journal of Radiology
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• 제23권2호
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• pp.189-201
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• 2022

Objective: To compare the outcomes of radiofrequency ablation (RFA) using dual switching monopolar (DSM), switching bipolar (SB), and combined DSM + SB modes at two different interelectrode distances (25 and 20 mm) in an ex vivo study, which simulated ablation of a 2.5-cm virtual hepatic tumor. Materials and Methods: A total of 132 ablation zones were created (22 ablation zones for each protocol) using three separable clustered electrodes. The performances of the DSM, SB, and combined DSM + SB ablation modes were compared by evaluating the following parameters of the RFA zones at two interelectrode distances: shape (circularity), size (diameter and volume), peritumoral ablative margins, and percentages of the white zone at the midpoint of the two electrodes (ablative margin at midpoint, AMm) and in the electrode path (ablative margin at electrode path, AMe). Results: At both distances, circularity was the highest in the SB mode, followed by the DSM + SB mode, and was the lowest in the DSM mode. The circularity of the ablation zone showed a significant difference among the three energy groups (p < 0.001 and p = 0.002 for 25-mm and 20-mm, respectively). All size measurements, AMm, and AMe were the greatest in the DSM mode, followed by the DSM + SB mode, and the lowest were with the SB mode (all statistically significant). The white zone proportion in AMm and AMe were the greatest in the SB mode, followed by the DSM + SB mode and DSM in general. Conclusion: DSM and SB appear to be complementary in creating an ideal ablation zone. RFA with the SB mode can efficiently eradicate tumors and create a circular ablation zone, while DSM is required to create a sufficient ablative margin and a large ablation zone.

• 한국진공학회:학술대회논문집
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• 한국진공학회 2016년도 제50회 동계 정기학술대회 초록집
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• pp.200.2-200.2
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• 2016

Carbon-based materials have been known as ablative material and have been used for thermal protection systems. Ablation is an erosive phenomenon that results in thermochemical and thermomechanical changes on materials. Ablation resistance is one of the key properties that determines performance and life-time of the thermal protection material under ablative conditions. In this study, ablation properties of graphite, 3-dimensional (C/C) composites (needle-punched type and rod type) were investigated byusing a plasma wind tunnel which produce a supersonic plasma flow from a segmented arc heater with the power level of 0.4 MW. The mass losses and surface roughness changes which contain main result of the ablation are measured. A morphological analysis ofthe carbon-based materials, before and after the ablation test, are performed through field emission scanning electron microscopy (FE-SEM) and non-contact 3D surface measuring system. Electronic balance and a portable surface roughness tester were used for evaluation of the recession and mass loss of the test samples.

• Composites Research
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• 제26권5호
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• pp.309-314
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• 2013

소량의 CNT 나노입자를 함유한 CNT-페놀 복합재료를 제조하여 삭마 효과를 확인하였다. CNT 함량을 0.1 wt%에서 0.3 wt%까지 증가시킴에 따른 인장, 압축 강도를 평가하고 삭마 저항성에 대한 차이를 분석하였다. 산소와 등유를 혼합하여 화염 발생시켜 재료의 삭마 효과를 평가하였다. FE-SEM을 이용하여 삭마 실험 이후 발생된 시편의 미세 구조 변화를 확인하였다. CNT 함유 정도에 따른 TGA 열분석을 시도하여 열적 안정성을 평가하였다. 0.3wt% CNT-페놀 복합재료가 일반 페놀 수지 및 0.1 wt% CNT-페놀 복합재료보다 삭마율이 낮았다. 삭마에 따른 재료 변화 메커니즘을 규명하기 위해 TGA 분석 결과와 FE-SEM을 이용한 미세 구조 결과를 분석하였다. 고열의 화염을 이용한 삭마 실험을 통해 시편 내부의 CNT 입자가 존재하는 미세구조를 확인할 수 있었다. 수지 내부에 균일하게 분산된 CNT 입자의 역할이 내삭마성을 증가시키는 결과를 확인하였다.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 1999년도 추계학술발표대회 논문집
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• pp.160-163
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• 1999

The mechanical properties and failure behaviour of carbon/phenolic composites were inverstigated by tension and compression. Carbon/phenolic composites were fabricated by infiltration of matrix into 8 harness satin woven fabric of PAN-based carbon fibers. The tensile and compressive tests were performed at 25℃ under air atmosphere and, at 400℃ and 700℃ under N₂ atmosphere. The tensile strengths of carbon/phenolic composites in with-laminar/0° warp direction were about 10 times higher than those in with-laminar/45° warp direction, which was analyzed due to a change of fracture mode from fiber pull-out by shear to tensile fracture of fibers. The fracture of carbon/phenolic composites in with-laminar/45° direction was analyzed due to delamination by buckling. Tensile and compressive strength of carbon/phenolic composites decreased to about 50% at 400℃, and to about 10% at 700℃ compared to that at room temperature. The main reason for the decrease of tensile or compressive strength with increasing temperature was analyzed due to a reduction of bond strength between fibers and matrix resulting from thermal degradation of phenolic resin.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2005년도 제24회 춘계학술대회논문집
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• pp.305-308
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• 2005

본 논문은 30ton급 액체로켓엔진 연소기의 연소시험 검증용 제작에 관한 것이다. 기본설계와 상세설계를 통해 도면을 작성하고, 이에 따라 제작하였다. 연소기는 크게 헤드부와 챔버부로 구성되며, 챔버는 KSR-III에 적용되었던 내열재 챔버와 재생 냉각 방식의 챔버를 제작하였다. 연소기 헤드는 저온 특성이 좋은 SUS316L 재료를 사용하였다. 내열재 챔버는 내부는 silica/phenolic 재료를 사용하였고, 외부케이스는 SUS316L을 적용하였고, 재생 냉각 챔버는 C18200과 SUS316L 재료를 사용하였다. 선반 가공, 일반 밀링 가공, MCT 가공등의 기계적 가공을 한 후 전해 연마를 통해 이물질을 제거 하였다. 분사기와 분사기 플레이트의 접합과 재생 냉각 챔버 등 일부 부품의 접합은 구조적인 특성으로 인해 브레이징 기법을 적용하였다.