• 한국전자파학회논문지
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• 제14권11호
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• pp.1207-1215
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• 2003

본 논문에서는 대수주기 다이폴 안테나(LPDA: Log-Periodic Dipole Antennas)의 크기를 줄이기 위해 다이폴 소자를 벤트 다이폴 소자로 대체한 대수주기 벤트 다이폴 안테나(LPBDA: Log-Periodic Bent Dipole Antennas)를 제안하였다. 1 ㎓∼3 ㎓ 사이에서 동작하는 LPBDA를 설계하고 모멘트법을 이용하여 복사특성을 해석하여 LPDA의 특성과 비교 검토하였다. 그 결과 본 논문에서 제시한 LPBDA는 다이폴 소자의 길이를 약 20% 줄이면서도 복사특성이 LPDA와 비교하여 거의 차이가 없는 것으로 나타났으며, 제작 측정한 LPBDA의 특성도 계산 결과에 근접했다.

• 한국전자파학회논문지
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• 제10권3호
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• pp.329-339
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• 1999

LPDA(Log-Periodic X Dipole Antenna)에 비하여 안테나 붐의 길이가 짧으면 서도 복사특성이 우수한 대수주기 안테나로서 X 다이폴을 구성소자로 하는 LPXDA(Log-Periodic X Antennas)를 제안하였다. 500MHz~1,000MHz에서 동작하는 LPXDA를 설계하고 모멘트법을 이용하여 설계안테나의 본사특성을 해석하여 LPDA의 특성과 비교 검토하였다. 그 결과 본 논문에서 제시한 LPXDA가 LPDA보다 붐의 길이가 20%짧으면서도 주파수 변화에 따른 복사특성이 우수한 것으로 나타났으며 LPXDA의 측정결과도 계산결과에 근접하는 것으로 나타났다.

• 한국전자파학회논문지
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• 제26권2호
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• pp.196-203
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• 2015

곡면 위상 배열 안테나나 곡면 주파수 선택 구조 등의 전파 특성을 해석하기 위해서는 원통형 배열 구조의 효율적인 해석방법에 대한 연구가 필요하다. 원통형 배열 구조가 실제 적용되는 구조는 유한 배열 구조지만, 대부분 전자기 해석은 무한 배열 구조라 가정하므로 실제 구조의 특성과 근사화한 구조의 특성 간의 오차가 발생하게 된다. 따라서 원통형 무한 배열 구조와 유한 배열 구조의 전파 특성의 비교와 분석이 필요하다. 본 논문에서는 원통형 무한 배열 구조를 해석하기 위해 원통형 Floquet harmonics 해석 방법을 적용하였으며, 원통형 유한 배열 구조를 해석하기 위해서는 너비가 좁은 스트립(strip)이 배열된 배열 구조를 가정하여 thin wire approximation을 적용한 method of moments(MoM)를 이용하였다. 본 논문에서는 원통형 유한 배열 구조와 무한 배열 구조의 전파 특성을 비교하기 위하여 투과 특성과 전류 분포를 계산하였다.

• 한국전자파학회논문지
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• 제21권9호
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• pp.1005-1012
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• 2010

본 논문에서는 대수 주기 코흐 다이폴 안테나(LPKDA: Log Periodic Koch Dipole Antenna)의 크기를 줄이기 위해 코흐 다이폴 소자를 칸토어 코흐 다이폴 소자로 대체한 대수 주기 칸토어 코흐 다이폴 안테나(LPCKDA: Log Periodic Cantor Koch Dipole Antenna)를 제안하였다. 제안된 안테나의 타당성을 확인하기 위하여 0.5~1.5 GHz의 주파수에서 동작하는 LPCKDA를 설계 및 제작하여 기존의 LPKDA(LPKDA: Log Periodic Koch Dipole Antenna)의 특성과 비교하였다. 그 결과, 본 논문에서 제안한 LPCKDA는 다이폴 소자의 길이를 약 5 % 줄이면서 복사 특성이 LPKDA와 비교하여 거의 차이가 없는 것으로 나타났다.

• 한국직업건강간호학회지
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• 제9권1호
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• pp.30-38
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• 2000

This study was carried out to investigate what factors affect satisfaction of periodic health examination undertaken by employees. The purpose of the study was to improve quality of periodic health examination and to increase the rate of workers participation in the screening test. The content of questionnaire was designed with focus on the satisfaction and attitude on the periodic health examination. Data were analyzed with 212 males, 181 females among 393 samples who took periodic examination at a general hospital in Seoul. Korea. The results were as follows: 1. Respondents were mainly in the thirties(42.7%), married(58.5%), more than 3 years working experiences(66.7%) and employed in Sales & Customers service industry(60.1%). 2. There were significant differences in the scores of satisfaction by general characteristics among the respondents. The highly educated and the single showed higher satisfaction on the periodic health examination than other respondents. 3. The scores of satisfaction in periodic health examination showed highly influenced by level of age, work duration, level of knowledge to the health screening and income. Based on the results, this study concluded that the periodic health examination might be necessary to modify its items according to the clients characteristics and their individual demands for maintenance of healthy life.

• Advances in aircraft and spacecraft science
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• 제4권4호
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• pp.353-369
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• 2017

Flutter is a dangerous phenomenon encountered in flexible structures subjected to aerodynamic forces. This includes aircraft, buildings and bridges. Flutter occurs as a result of interactions between aerodynamic, stiffness, and inertia forces on a structure. In an aircraft, as the speed of the flow increases, there may be a point at which the structural damping is insufficient to damp out the motion which is increasing due to aerodynamic energy being added to the structure. This vibration can cause structural failure, and therefore considering flutter characteristics is an essential part of designing an aircraft. Scientists and engineers studied flutter and developed theories and mathematical tools to analyze the phenomenon. Strip theory aerodynamics, beam structural models, unsteady lifting surface methods (e.g., Doublet-Lattice) and finite element models expanded analysis capabilities. Periodic Structures have been in the focus of research for their useful characteristics and ability to attenuate vibration in frequency bands called "stop-bands". A periodic structure consists of cells which differ in material or geometry. As vibration waves travel along the structure and face the cell boundaries, some waves pass and some are reflected back, which may cause destructive interference with the succeeding waves. This may reduce the vibration level of the structure, and hence improve its dynamic performance. In this paper, for the first time, we analyze the flutter characteristics of a wing with a periodic change in its sandwich construction. The new technique preserves the external geometry of the wing structure and depends on changing the material of the sandwich core. The periodic analysis and the vibration response characteristics of the model are investigated using a finite element model for the wing. Previous studies investigating the dynamic bending response of a periodic sandwich beam in the absence of flow have shown promising results.

• Advances in aircraft and spacecraft science
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• 제6권1호
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• pp.31-49
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• 2019

Flutter is a dangerous phenomenon encountered in flexible structures subjected to aerodynamic forces. This includes aircraft, helicopter blades, engine rotors, buildings and bridges. Flutter occurs as a result of interactions between aerodynamic, stiffness and inertia forces on a structure. The conventional method for designing a rotor blade to be free from flutter instability throughout the helicopter's flight regime is to design the blade so that the aerodynamic center (AC), elastic axis (EA) and center of gravity (CG) are coincident and located at the quarter-chord. While this assures freedom from flutter, it adds constraints on rotor blade design which are not usually followed in fixed wing design. Periodic Structures have been in the focus of research for their useful characteristics and ability to attenuate vibration in frequency bands called "stop-bands". A periodic structure consists of cells which differ in material or geometry. As vibration waves travel along the structure and face the cell boundaries, some waves pass and some are reflected back, which may cause destructive interference with the succeeding waves. In this work, we analyze the flutter characteristics of a helicopter blades with a periodic change in their sandwich material using a finite element structural model. Results shows great improvements in the flutter forward speed of the rotating blade obtained by using periodic design and increasing the number of periodic cells.

• Journal of electromagnetic engineering and science
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• 제1권2호
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• pp.161-165
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• 2001

The radiation characteristics of leaky wave emanated from finite strip-grating loaded dielectric coated coaxial waveguide with finite periodic thick slots are investigated theoretically. The rigorous integral equations are derived for the proposed structure using the courier transform, mode expansion, and sine series expansion of the electric current on metallic strips, and the simultaneous linear equations are obtained. The effects of finite strip-grating loading on a dielectric-coated coaxial waveguide with finite periodic thick slots are examined in terms of radiation characteristics.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 1997년도 춘계학술대회논문집; 경주코오롱호텔; 22-23 May 1997
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• pp.49-54
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• 1997

In this paper, vibration characteristics are considered about thermo-visco-plastic material under periodic thermal loading. When in high temperature region, thermo-visco-plastic structure has a periodic thermal loading, it is very important in an accumulated structure like a spacestation to investigate vibration characteristic, stress-strain characteristic is considered in various 2-D model by finite element method.

• 대한기계학회논문집
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• 제19권9호
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• pp.2173-2180
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• 1995

This paper presents free vibration analysis method using the characteristics of the rotationally periodic structures and includes the analysis results of a tire as an example. The normal modes of the rotationally periodic structures are the kind of standing waves, so all sectors have the same deflection shapes, and only different phases. This property makes it possible to derive the analysis method called sector method. The sector method can give the accurate natural frequencies and the corresponding mode shapes of the rotationally periodic structure with information of only one sector. When the free vibration analysis is performed to find the dynamic characteristics of the rotationally periodic structure by using the sector method, the computer memory spaces and the CPU times can be saved. We obtained much economic benefits by using the sector method in the analysis of dynamic characteristics of a tire made of non-linear materials.