• 만화애니메이션 연구
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• 통권27호
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• pp.1-30
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• 2012

오시이 마모루에 대한 연구는 대체로 그의 작품들이 현실의 황폐함을 '폐허'의 이미지로 재현하고 있다는데 집중해 왔다. 또 오시이 마모루의 애니메이션이 점점 디자인적으로 '현실미'를 드러내기 위해 발전해 갔다고도 주장해 왔다. 그러나 본 연구는 그의 작품이 근대적 자본주의의 억압된 '현대세계'를 벗어날 수 있는, 전복의 가능성을 모색하고 있음에 주목하고자 한다. 이를 위해 <스카이 크롤러>(The Sky Crawlers)를 공간, 신체, 일상성 세 가지 층위로 나누어 분석했다. 2장에서는 <스카이 크롤러>의 공간이 근대적이고 기계적인 빈틈없이 자본화된 공간이자 '반복'의 성질을 지닌 폐쇄된 회로와 같은 공간임을 분석했다. 3장에서는 캐릭터 신체의 측면에서 <스카이 크롤러>가 '키르도레'(Kildren)라는 인간과 비인간의 사이에서 유동하는 신체를 제시하고 있으며 이를 통해 현대세계의 자본화되고 물화된 신체를 재현하고 있다고 분석했다. 또 그 신체가 처한 극단적 불안이 현대세계의 노동 유연화에 따른 '불안'과 '장소상실' 현상을 반영하고 있음을 밝혀 보았다. 4장에서는 미장센과 디자인 그리고 연출의 측면에서 현대세계의 '일상성'이 신체에 남긴 '기억'과 '습관'의 측면을 분석했다. 5장에서는 이런 현대세계에 대한 현실 인식을 바탕으로 오시이 마모루가 근대공간에서 어떻게 '도주'하고자 하는가를, 근대적 일상을 어떻게 '전유'하려 하는지를 살펴보았다. 6장 결론에서는 이러한 오시이 마모루의 작품이 지닌 의미와 가치를 해석해 보았다.

• 한국지구물리탐사학회:학술대회논문집
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• 한국지구물리탐사학회 2010년도 학술대회 초록집
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• pp.39-42
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• 2010

• 대한치과교정학회지
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• 제47권6호
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• pp.344-352
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• 2017

Objective: The purpose of this study was to compare the changes induced in the pharyngeal airway space by orthodontic treatment with bodily retraction of the mandibular incisors and mandibular setback surgery without extraction. Methods: This retrospective study included 63 adult patients (32 men and 31 women). Thirty-three patients who had been treated via four-bicuspid extraction and bodily retraction of the mandibular incisors (incisor retraction, IR group) were compared with 30 patients who had been treated via mandibular setback surgery (MS group) without extraction. Lateral cephalograms were acquired and analyzed before (T1) and after treatment (T2). Results: The superior pharyngeal airway space did not change significantly in either group during treatment. The middle pharyngeal airway space decreased by $1.15{\pm}1.17mm$ and $1.25{\pm}1.35mm$ after treatment in the IR and MS groups, respectively, and the decrease was comparable between the two groups. In the MS group, the inferior pharyngeal airway space (E-IPW) decreased by $0.88{\pm}1.67mm$ after treatment (p < 0.01). The E-IPW was larger in the MS group than in IR group at T1, but it did not differ significantly between the two groups at T2. No significant correlation was observed between changes in the pharyngeal airway space and the skeletal and dental variables in each group. Conclusions: The middle pharyngeal airway space decreased because of the posterior displacement of the mandibular incisors and/or the mandibular body. The E-IPW decreased only in the MS group because of the posterior displacement of only the mandibular body.

• 대한치과보철학회지
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• 제43권5호
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• pp.622-632
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• 2005

Statement of problem: Silicone Index Tooth Tray impression system which does not use gingicord has a shortcoming. It takes time to remove internal wall of Silicone Index Tooth Tray for space of wash impression material. Purpose: This study was to evaluate whether providing certain space to impression body can prevent from doing complicated laboratory work. Material and methods: After mounting metal dies with shoulder and chamfer margins arbiturarily, SITT was produced using $Blu-mousse^(R)$. In one experimental group, wash impression was taken using $Fit-tester^(R)$ without removing interior surface of SITT and in the other group, wash impression was taken using $Fit-tester^(R)$ providing 0.5mm space in the SITT and then compared the differences in two groups. Results: 1. There was no significant difference between a group which did not allow space and a group which granted equal 0.5mm space. 2. There was no significant difference between gingival diameter, occlusal diameter of metal die that has shoulder margin and gingival diameter, occlusal diameter of metal die that has chamfer margin. 3. There was no significant difference between a group which did not take pick-up impression and a group which took pick-up impression through relining method using SITT 4. There was no significant difference between a group that poured immediately after taking primary impression and a group that poured after removing poured stone die. Conclusions: When taking an impression of an abutment using SITT impression system, it is considered to obtain clinically identical results between a group that did not grant a 0.5mm space within SITT for wash impression and a group which invest a space. Furthermore, it is considered possible to produce an individual die through secondary pouring.

• 우주기술과 응용
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• 제1권2호
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• pp.149-159
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• 2021

본 논문은 2021년 5월에 수행된 국제우주쓰레기조정위원회(IADC, Inter-Agency Space Debris Coordination Committee Reentry) 재진입 테스트 캠페인의 분석 대상인 중국 창정 5B호 발사체의 재진입 시점 예측 분석 내용을 포함하고 있다. 우주물체의 재진입 예측은 물체의 크기나 무게, 자세에 대한 정확한 정보의 부재, 대기밀도의 불확실성 등으로 정확한 예측이 어렵다. 때문에 IADC에서는 재진입 캠페인을 매년 수행하여 기관별 분석기법에 대한 검증을 수행하고 있고, 한국항공우주연구원에서도 2015년부터 이에 참여하고 있다. 본 연구에서는 우주물체가 재진입하는 시점을 예측하기 위해 탄도계수 최적화 기법을 제안하였고, 이를 활용하여 분석 대상의 재진입 시점을 예측한 결과, 실제 재진입 시점과 약 73초의 차이를 보여주어 제안한 기법의 정확도를 확인하였다.

• International Journal of Aeronautical and Space Sciences
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• 제16권2호
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• pp.295-310
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• 2015

In the present study, an unstructured mixed mesh flow solver was used to conduct a numerical prediction of the aerodynamic performance of the S-76 rotor in hover. For the present mixed mesh methodology, the near-body flow domain was modeled by using body-fitted prismatic/tetrahedral cells while Cartesian mesh cells were filled in the off-body region. A high-order accurate weighted essentially non-oscillatory (WENO) scheme was employed to better resolve the flow characteristics in the off-body flow region. An overset mesh technique was adopted to transfer the flow variables between the two different mesh regions, and computations were carried out for three different blade configurations including swept-taper, rectangular, and swept-taper-anhedral tip shapes. The results of the simulation were compared against experimental data, and the computations were also made to investigate the effect of the blade tip Mach number. The detailed flow characteristics were also examined, including the tip-vortex trajectory, vortex core size, and first-passing tip vortex position that depended on the tip shape.

• 한국실내디자인학회논문집
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• 제16권1호
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• pp.48-55
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• 2007

Proceedings in a new field of sciences and technologies like genetic engineering challenge to conventional concepts. It demonstrates a certain disappearance in conventional concepts that dominants our perceptions, such as organic, mechanical, and dichotomic concept of informative materials, and that is to be extended as a potential possibility. Then, what is a new space where our bodies that feel and cherish in their mind should live in these days as well as it makes senses by itself and should affect the principle that makes worlds? In addition, this study proposes a frame in the analysis in order to understand a section of modern designs with the question of 'what is the change in the relationship between relative structures in spaces and objects from a design point of view according to new structural concepts of body?' The major point of this analysis can be realized based on the assumption of the extension of the characteristics in the change of structural relationship in the aspect of post structuralism that includes non-structuralized relationship represented in modern philosophy, arts, and architectural works. Then, it can be accomplished as positive ideas in the foundation of space designs in future including the understand of 'new structural relationship' that can't be expressed as rationality and causal sequence by considering how the experiment conducted using several topics on body can be projected onto spaces through the process applied in the experiment.

• International Journal of Aeronautical and Space Sciences
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• 제8권2호
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• pp.67-75
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• 2007

An attitude control problem for a tethered spacecraft is studied. The tethered spacecraft is viewed as a multi-body spacecraft consisting of a base body, a massless tether that connects the base body and an end mass, and tether actuator dynamics. Moments about the pitch and roll axes of the base spacecraft arise by control of the point of attachment of the tether to the base spacecraft. The control objective is to stabilize the attitude of the base spacecraft while keeping the perturbations of the tether small. Analysis shows that linear equations of motion for the tethered spacecraft are not completely controllable. We study two different control design approaches: (1) we decouple the attitude dynamics from the tether dynamics and we design a linear feedback to achieve stabilization of the attitude dynamics, and (2) we decouple the controllable modes from the uncontrollable mode using Kalman decomposition and we design a linear feedback to achieve stabilization of the controllable modes. Simulation results show that, although it is difficult to control the tether, the tether motion can be maintained within an acceptable range while stabilizing the attitude dynamics of the base spacecraft.

• 한국항공우주학회지
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• 제33권8호
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• pp.42-49
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• 2005

아음속풍동 폐쇄형 시험부의 벽면효과 보정을 위한 새로운 blockage 보정 기법을 개발하였다. 개발된 보정 기법은 실속항력계수와 separation blockage의 비선형 관계를 이용하여 선형 양력곡선 기울기 영역에서 후실속 영역까지 실시간으로 보정이 가능하게 하였다. 본 연구에서 제시한 방법은 bluff body 시험 결과를 사용하는 고전적 방법과 벽면압력측정 방법과 비교하여 그 타당성을 검증하였다. 그 결과 본 연구에서 제시한 보정 방법은 실속 및 후실속 영역에서 bluff body 방법보다 우수한 보정 결과를 보이며 벽면압력측정 방법과 같은 정확도로 보정됨을 확인할 수 있었다.

• International Journal of Aeronautical and Space Sciences
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• 제17권2호
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• pp.139-148
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• 2016

The passive control methods such as horizontal and vertical fences on the lower surface of the bluff body were applied to suppress the vortex shedding and enhance the aerodynamic stability of flow. For investigating the effects of the passive control methods, wind tunnel experiments on the unsteady flow field around a bluff body near a moving ground were performed. The boundary layer and velocity profiles were measured by the Hot Wire Anemometer (HWA) system and the vortex shedding patterns and flow structures in a wake region were visualized via the Particle Image Velocimetry (PIV) system. Also, it is a measuring on moving ground condition that the experimental values of the critical gap distances, Strouhal numbers and aerodynamic force FFT analyses. Through the experiments, we found that the momentum supply due to moving ground caused the vortex shedding at the lower critical gap distance rather than that of fixed ground. The horizontal and vertical fences increase the critical gap distance and it can suppress the vortex shedding. Consequently, the stability characteristics of the bluff body near a moving ground could be effectively enhanced by the simple passive control such as the vertical fences.