• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2015.05a
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• pp.168-169
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• 2015

금속 박막과 폴리머 기판 사이에 접착력을 증대시키는 방법으로 금속-폴리머 계면에 나노 임프린트 구조체를 이용하는 방식을 최초로 이용하였다. 나노선 어레이 형상을 가진 몰드와 열 임프린트 방식을 이용하여 폴리머 기판 표면 위에 나노선 어레이 형상을 임프린트 하고, 열 증착 방식으로 금속 박막을 올렸다. 본 연구에서 제작된 금속-임프린트 폴리머 계면에서 높은 기계적 굽힘성 및 접착력을 가지는 것을 확인하였다.

• Proceedings of the Korea Contents Association Conference
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• 2006.11a
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• pp.801-805
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• 2006

In this paper, we describe a system of controlling the pictorial puzzle program using information of hand shape. We extract hand region using skin color information and then principal component analysis uses centroidal profile information which comes blob of 2D appearance for hand shape recognition. This method suit hand shape recognition in real time because it extracts hand region accurately, has little computation quantity, and is less sensitive to lighting change using skin color information in complicated background. Finally, we controlled a pictorial puzzle with using recognized hand shape information. This method has good result when we make an experiment on application of pictorial puzzle. Besides, it can use so many HCI field.

• Bulletin of the Korean Space Science Society
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• 2003.10a
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• pp.74-74
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• 2003

로켓엔진의 연소실에서는 고온의 연소가스로부터 다량의 열이 발생하기 때문에 이로부터 연소실을 보호하기 위한 방법이 필수적으로 요구된다. 한국 최초의 액체 로켓인 KSR-III 로켓의 주엔진인 KL-3 엔진에서는, 연소실을 보호하기 위한 방법으로 실리카/페놀(Silica/Phenolic) 내열재를 이용하는 용융냉각 방식을 채택하였다 용융냉각 방식은 내열재와 고온의 연소가스와의 물리ㆍ화학적 상호작용에 의해 삭마가 발생하게 되는데, 이러한 삭마는 연소실에서도 가장 고온부인 노즐목에 집중적으로 발생하는 경향이 있다. 그러나 노즐목에서 삭마의 진행은 노즐목의 크기를 증가시키고 연소압 및 추력을 감소시키는 부작용을 초래하게 된다. 본 연구에서는 이러한 열적 삭마에 의한 노즐목 크기의 증가량을 알아내기 위해 KL-3 엔진 노즐목의 형상을 측정하고자 시도하였으며, 노즐목의 삭마에 영향을 미치는 주요 인자를 확인하고 진행과정을 고찰하였다. 노즐목의 형상 측정을 위해서는 기존에 사용하던 3차원 변위 측정기를 이용한 방식의 접근이 곤란함에 따라 영상처리 기법을 도입한 측정 방식을 고안하여 사용하였으며, 이 장비는 만족스런 성능을 보여주었다. 시험결과를 통해서 삭마에 영향을 주는 주요 인자로 분무형태, 연소시간, 연소 온도를 제시하였고 이 중에서 분무형태는 삭마 형상에, 연소 시간 및 연소온도는 삭마량에 주로 영향을 끼친다는 것을 알 수 있었다. 또한 시간에 따른 삭마의 진행이 3개의 구간으로 나누어 설명할 수 있음을 밝혔는데, 노즐목이 원형을 그대로 유지하며 삭마진행이 미미한 구간, 원형에서 벗어나 요철형상이 발달하면서 삭마진행이 가속되는 구간, 요철형상이 이미 정착되어서 요철의 깊이만 증가하되 삭마량은 미미한 구간이다. 결과적으로 60초 연소 후 노즐목 면적 증가율은 +5.82% 정도이며, 이에 따른 연소압 및 추력의 감소 또한 1% 미만으로 미비하였다. 따라서 본 KL-3 엔진에 사용된 내열재의 내열 성능은 임무를 수행하기에 적절하다고 판단하였다.

• Journal of the Institute of Electronics Engineers of Korea SP
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• v.41 no.6
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• pp.137-145
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• 2004

The general software configuration management system shows lack of the properties and features of software development environment for multimedia due to its wide range to be covered. Multimedia software development environment has properties like repetitive analysis and simulation using visual programming environment where, beside support of elementary development functions, component or library can be combined and tested interactively. Moreover, the method to look fast and effective for component having similar function is required. In this paper, we present the system which supports the software configuration management method for a simulation tool and the system for the properties in the multimedia software development environment. And we relate our system to real simulation tool so as to check its ability as the software configuration management system for multimedia software development environment.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.1153-1155
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• 2017

The Launch Vehicle is made up of one system with several parts gathered together. In order to make the various parts developed in various organizations into one system, it is necessary to confirm all designs at certain point in time. Change after the design fix require controlled process to analyze the impact of the changes, to decide whether or not to make the change, and to verify that the change was implemented as intended. The configuration management procedure implemented in the above manner is also applied to the development process of KSLV-II. The CAD tool and PLM are linked with each other to perform configuration management for the 3D model, 2D drawing, and the configuration identification document.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2011.04a
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• pp.35-38
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• 2011

Damping characteristic according to acoustic cavity's geometries was investigated to control the high frequency combustion instability occurring in the Liquid Rocket Combustion Chamber by experimental test and linear analysis. Its diameter was determined as a design parameter and its orifice length and diameter were appointed as fixed parameter in this study. Result shows that the damping capacity has been almost constant through all the experiments despite using the same orifice and helmholtz resonators which have different volume.

• Journal of the Society of Naval Architects of Korea
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• v.31 no.3
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• pp.31-37
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• 1994

When a lot of input data are not distributed uniformly n a chord-span direction or when the given shape is complicated, it is very difficult to obtain an inverse matrix which represents the smooth Bi-cubic B-spline surface of the initial shape. To overcome this problem, we suggest image Surface Expansion Method(ISE Method) which is suggested for vertex creation of B-spline curves and surfaces. Its basic concept, convergency and verification are shown. Also B-spline curves and Surfaces represented by ISE Method were compared with those represented by the existing method which is based on the inverse matrix method, the pseudoinverse matrix method and the chord length approximation method for vertex yielding. Ship Hull Forms which have Knuckle, Bulbous Bow, Transom and Stern frame were represented by the ISE Method.

• The Journal of the Acoustical Society of Korea
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• v.29 no.7
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• pp.422-430
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• 2010

The radiation property of a Tonpilz transducer is influenced by the structural variables of the transducer. In this study, with respect to a single mode Tonpilz transducer, the radiation patterns were calculated for different head mass geometries of the same effective radiation area. The shapes of the head mass analyzed were the most popular circular, regular triangular, square, regular hexagonal and regular octagonal types, and radiation pattern equations were derived for each of the head mass shapes. Based on the derived equations, radiation patterns in accordance with the shape and size of the head mass were calculated and the results were compared with each other. Validity of the calculation results were confirmed by means of finite element analysis.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.18 no.9
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• pp.1-8
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• 2017

The purpose of this study is to propose a cache structure for processing large-volume building information modeling (BIM) geometry data,whereit is difficult to allocate physical memory. As the number of BIM orders has increased in the public sector, it is becoming more common to visualize and calculate large-volume BIM geometry data. Design and review collaboration can require a lot of time to download large-volume BIM data through the network. If the BIM data exceeds the physical free-memory limit, visualization and geometry computation cannot be possible. In order to utilize large amounts of BIM data on insufficient physical memory or a low-bandwidth network, it is advantageous to cache only the data necessary for BIM geometry rendering and calculation time. Thisstudy proposes acache structure for efficiently rendering and calculating large-volume BIM geometry data where it is difficult to allocate enough physical memory.

• The KIPS Transactions:PartB
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• v.12B no.1 s.97
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• pp.1-8
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• 2005

The importance of software is getting high in development of the digital device (digital camcoder, digital camera, mp3 player, ....). And because the sire of software becomes larger and complicated, the necessity of software configuration management (to solves a software crisis) is increased. The general software configuration management system shows lack of the property and features of software development environment for image processing algorithm due to its wide range to be covered. Image processing algorithm development environment has properties like repetitive analysis and simulation using visual programming environment where, beside support of elementary development functions. component(or library) can be combined and tested interactively. Moreover, the method to look fast and effectively for component having similar function is required. In this paper, we present the system which supports the software configuration management method for a simulation tool and the property in the visual programming environment. And we relate our system to real simulation tool so as to check its ability as the software configuration management system for image processing algorithm development environment.