• 디자인학연구
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• 제13권
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• pp.55-64
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• 1996

복식은 조형예술의 한 분야로 인간이 착용함으로써 생명력이 있는 형태를 이루고 인체를 기준으로 하는 입체성을 지닌 공간 조형이다. 그러므로 '옷을 입는다' 라는 단순한 차원을 넘어 인체의 움직임에 의해 나타나는 동감(動感)에 따라 입체적 형태를 이루는 조형성이 복식 디자인의 중요한 요소를 이루게 되었다. 이에 본 연구는 단순한 구조이면서도 인체의 동작과 착장 법에 의해 풍부한 공간감을 살릴 수 있는 관두의를 이론적으로 고찰하였다. 또한 간결하고 현대적인 특징을 지닌 기하학적 도형의 복합 형태 모티브로 한 관두의 형식의 복식 디자인을 연구하였다. 본 연구의 목적은 평면 패턴이 인체에 입혀졌을 때 형성되는 평면성과 입체성의 조화를 추구하며, 착장 법에 의한 기하학적인 면의 자연스러운 분할과 미묘한 색채 및 형태의 구성을 시도하여 보다 더 현대적이며 다양한 가변성(可變性)을 지닌 조형의상을 연구하는데 있다. 작품은 관두의 형식의 T자구조를 토대로 패턴을 구성하여 인체에 직접 입혀 형성되는 조형적 형태를 실험을 통해 실물 작품으로 제작하였다.

• 복식
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• 제56권1호
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• pp.121-130
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• 2006

Superimposition is a transforming technique that can facilitate the creation. Superimposition in previous studies, however, has only been fragmentary described as an expression technique, so the studies have not been conducted on the basis of its aesthetic value. The purpose of this study is to investigate how superimposition is applied and expressed in terms of forms of modern fashion based on multi-dimensional features of design processing. The codes of togetherness, ambivalence, sense of space and tension in dress were determined by using the expressional Superimposition. The forms of superimposition were limited to superimposition of clothing, superimposition of body and clothing and superimposition of body and Phenomenal body. This study found that superimposition has developed, in fashion forms/types, a new 'form' by overlapping various forms and thus provides a visual shock and a sense of mystery by using mismatched and arbitrary properties among the forms. Such a superimposition influences a methodology of fashion design through a designer's subjective tendencies, as well as influences a change in the view of the world. Also, a superimposition is expected to have a definite influence on new fashion trends.

• 한국항공우주학회지
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• 제36권12호
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• pp.1229-1235
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• 2008

비상위치송신기(ELT)는 무수한 조난시의 응급구조에 큰 역할을 해왔다. 비행사, 항해사 그리고 지상 사용자들은 세상 어디에서든지 비상시에 조난신호를 위성에 송신이 가능한 장치를 갖추고 있는 것이다. 이 논문에서는 비상위치송신기의 본체를 낙하충격에 대하여 MSC/Dytran을 이용하여 해석하였다. 그리고 그 결과를 Karas' Example 이론 결과에 비교하였다. 또한, 추락생존성 시험에 대해 MSC/Nastran을 이용해 해석하였다. 비상위치송신기의 충격조건하에 과도응답해석을 하였다.

• 한국의상디자인학회지
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• 제1권1호
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• pp.91-107
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• 1999

The primary purpose of this study is to inquire into the characteristic of exposure presented in fashion, identify the correct concept of exposure from an aesthetic perspective, and grasp the contemporary meaning of exposure presented in fashion. As a result of study, the following findings were obtained: First, the surrealist style of fashion exhibited representations such as the relocation of the partial details, the harmonization of the natural and the artificial, the emphasis or expansion of each part of the body, and the like. It used highlighted the genital region with ornamentations or used the technique of paradoxically exposing the part of the body always covered. And it exbibited the paradoxical relationship of exposure and concealment by exposing the concealed part of the human body. Second, the post-modern style showed the complicated phenomenon that the values of several meanings such as the historic, the folk, and the like appeared in its fashion. It shares in spatiotemporal eclecticism, pluralistic characteristics and the like found in the post-modern culture. Third, the deconstructive style gets rid of the distinction between the external space and the private space by translating underwears into outer garments. It destroys clothing by tearing or perforating clothing whereby it represents the poor image. Coupled with women‘s psychology of exposure and the new generation’s way of thinking indifferent to others‘ eyes, this fashion of deconstruction occupies the great current of fashion. Deconstructive fashion gets away with the rule of ‘having to wear clothing to suit TPO(Time, Place and Occasion), the traditional norm of wearing clothing.

• 한국지반공학회:학술대회논문집
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• 한국지반공학회 2005년도 지반공학 공동 학술발표회
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• pp.84-91
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• 2005

In case of soil nailing system, there have been many attempts to expand into slope and temporary earth retaining system stabilization method since the first ground excavation earth retaining system construction in 1993. Recently, jointing wall, underground wall of buildings and excavation earth retaining wall, construction were increasingly applied for effective utilization of the limited underground space and land application maximized. However, the application of joining wall into retaining wall or building by temporary soil nailing system and design of permanent wall were performed by using Rankine earth pressure theory without considering the distribution of earth pressure in the soil nailing. In this study was performed to introduce the design case by 'Two-Body Translation mechanism (TBTM)' to be able to consider distribution of earth pressure in the soil nailing when designing the permanent jointing wall using soil nailing system for effective utilization of ground space. Also, this study attempts to evaluate the earth pressure change, decreasing effect of wall displacement and increasing effect of stability when advanced soil nailing system is constructed using $FLAC^{2D}$ ${\nu}er.$ 3.30 program and 'Two-Body Translation mechanism'.

• International Journal of Naval Architecture and Ocean Engineering
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• 제9권6호
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• pp.693-704
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• 2017

Blended-Wing-Body Underwater Glider (BWBUG), which has excellent hydrodynamic performance, is a new kind of underwater glider in recent years. In the shape optimization of BWBUG, the lift to drag ratio is often used as the optimization target. However this results in lose of internal space. In this paper, the energy reserve is defined as the direct proportional function of the internal space of BWBUG. A motion model, which relates gliding range to steady gliding motion parameters as well as energy consumption, is established by analyzing the steady-state gliding motion. The maximum gliding range is used as the optimization target instead of the lift to drag ratio to optimizing the shape of BWBUG. The result of optimization shows that the maximum gliding range of initial design is increased by 32.1% though an Efficient Global Optimization (EGO) process.

• 한국항공우주학회지
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• 제42권3호
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• pp.213-220
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• 2014

본 연구에서는 헬리콥터의 간섭유동장을 고려한 발사체의 궤적예측 프로그램을 개발하였다. 헬리콥터의 간섭유동장 해석에는 엑츄에이터 디스크 모델이 적용된 압축성 비점성 해석자를 이용하였다. 발사체의 궤적 해석에는 6자유도 운동방정식과 대안적 형태의 수정된 질점 운동방정식을 사용하였다. 헬리콥터 주위 유동 해석은 ROBIN(ROtor Body INteraction) 모델을 이용하여 검증하였다. Sierra International 탄과 105mm 포탄의 궤적을 이용해 운동 해석 모듈을 검증하였다. 헬리콥터에서 발사된 발사체의 궤적 예측에는 Sierra International 탄과 HYDRA 70 로켓을 이용하였다.

• 지구물리와물리탐사
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• 제14권2호
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• pp.133-139
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• 2011

지구조석을 계산하는데 있어 가장 주요한 항은 달이나 태양에 의한 구면조화차수가 2인 항으로서 지구조석의 약 98%를 이루며, 나머지는 3차 이상의 고차 항들이다. 그런데 차수 3항과 그 이상의 고차수의 항들의 값들은 차수 2항과는 다른 상수가 각각 곱하여져서 계산되어야 한다. 본 연구에서는 조석에 의한 중력변화, 변위 및 수직선의 변화에 대한 바른 계산을 검토하였으며, 필요한 관련상수들을 다시 구하였다. 동일차수내의 다른 계수의 조화함수적 조석주기의존성을 토의하였다. 한편, 지구조석을 계산하는데 관련된 중요한 개념들을 요약 소개하였다.

• International Journal of Aeronautical and Space Sciences
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• 제16권3호
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• pp.394-406
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• 2015

In this work, an efficient aircraft landing simulation strategy is proposed to develop an efficient and reliable hard-landing monitoring procedure. Landing stage is the most dangerous moment during operation cycle of aircraft and it may cause structural damage when hard-landing occurs. Therefore, the occurrence of hard-landing should be reported accurately to guarantee the structural integrity of aircraft. In order to accurately determine whether hard-landing occurs or not from given landing conditions, full nonlinear structural dynamic simulation can be performed, but this approach is highly time-consuming. Thus, a more efficient approach for aircraft landing simulation which uses a hierarchical aircraft landing model and an extended inertia relief technique is proposed. The proposed aircraft landing model is composed of a multi-body dynamics model equipped with landing gear and tire models to extract the impact force and inertia force at touch-down and a linear dynamic structural model with an extended inertia relief method to analyze the structural response subject to the prescribed rigid body motion and the forces extracted from the multi-body dynamics model. The numerical examples show the efficiency and practical advantages of the proposed landing model as an essential component of aircraft hard-landing monitoring procedure.

• International Journal of Aeronautical and Space Sciences
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• 제9권1호
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• pp.121-128
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• 2008

This paper describes the modeling and autopilot design procedure of a Blended Wing-Body(BWB) UAV. The BWB UAV is a tailless design that integrates the wing and the fuselage. This configuration shows some aerodynamic advantages of lower wetted area to volume ratio and lower interference drag as compared to conventional type UAV. Also, BWB UAV may be increase payload capacity and flight range. However, despite of these benefits, this type of UAV presents several problems related to flying qualities, stability, and control. In this paper, the detailed modeling procedure of BWB UAV and stability analysis results using the linearized model at trim condition are represented. Finally, we designed the autopilot of BWB UAV based on a simple control allocation scheme and evaluated its performance through nonlinear simulation.