• Steel and Composite Structures
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• 제47권3호
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• pp.437-450
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• 2023

A half open cross section built-up column, namely cold-formed thin-walled steel built-up column with 12-limbsection (CTSBC-12) is put forward. To deeply reveal the mechanical behaviors of CTSBC-12 under axial compression and put forward its calculation formula of axial bearing capacity, based on the previous axial compression experimental research, the finite element analysis (FEA) is conducted on 9 CTSBC-12 specimens, and then the variable parameter analysis is carried out. The results show the FEA is in good agreement with the experimental research, the ultimate bearing capacity error is within 10%. When the slenderness ratio is more than 96.54, the ultimate bearing capacity of CTSBC-12 decreases rapidly, and the failure mode changes from local buckling to global buckling. With the local buckling failure mode unchanged, the ultimate bearing capacity decreases gradually as the ratio of web height to thickness increases. Three methods are used for calculating the ultimate bearing capacity, the direct strength method of AISI S100-2007 gives result of ultimate axial load which is closest to the test and FEA results. But for simplicity and practicality, a simplified axial bearing capacity formula is proposed, which has better calculation accuracy with the slenderness ratio changing from 30 to 100.

• 전력전자학회:학술대회논문집
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• 전력전자학회 2019년도 전력전자학술대회
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• pp.301-302
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• 2019

ITER CS, VS, CC AC/DC Converter는 4상한 동작을 하며, PCS(Plasma Control System)에서 명령하는 출력 전압 제어를 컨버터 교류 입력 전압 변동을 보상하는 Feed-forward 방식을 사용한다. Feed-forward 제어를 위하여 교류 입력 전압에 대한 실시간 정밀 측정이 가능한 RMS 계산이 필요하다. 본 논문은 RMS 연산에 대한 개선된 방법을 제안하면서 시뮬레이션과 실험을 통해 해당 알고리즘을 검증하였고 이에 대한 내용을 논의하고자 한다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 추계학술대회논문집B
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• pp.312-317
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• 2001

Modifying effects of the rectangular forward step for suppressing the unsteady pressure fluctuation during interaction between the upstream vortical flow with the edge are studied numerically. The vortical flow is modeled by a point vortex, and the unsteady pressure coefficient is obtained from the velocity and the potential field. To investigate the effects of the edge shape the rectangular forward step is chamfered with various angles. Calculation show that the pressure peaks become decreased by increasing the vortex height as well as the chamfering angle. The pressure amplitudes are very sensitive to the change of the initial vortex height. From this study we can find out that the chamfered edge has two effects; the one is that it suppresses the pressure amplitude generated from the edge, and the other is that it decreases the time variation of unsteady pressure fluctuation. These modifying concepts can be applied to attenuate the self-sustained oscillation mechanism at the open cavity flow.

• 대한조선학회논문집
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• 제56권5호
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• pp.396-409
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• 2019

In this paper, a comparative study on the radiation techniques for the motion analysis of the three dimensional floating structure with the forward speed was carried out. The Sommerfeld radiation condition, the damping technique, and the point shift technique were used for the comparative study. Radiated wave patterns and hydrodynamic coefficients of the heave motion of floating structure with the forward speed were compared and analyzed. The characteristics and limitations of each radiation technique were analyzed through the calculation results. To overcome the limitations of conventional radiation techniques, the hybrid radiation technique combining the Sommerfeld radiation condition with the damping technique was proposed. It is confirmed that the proposed method, the Hybrid radiation technique, improves the limitation of the speed range and the dissipation of the wave of the conventional radiation technique. The motion analysis code of the three dimensional floating structure with the forward speed based on the Rankine source method with hybrid radiation technique was developed. In order to validate the developed code, hydrodynamic analyses were carried and compared with published experiments.

• 항공우주기술
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• 제1권2호
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• pp.1-10
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• 2002

본 연구에서는 전진익 소형기 항공기 형상에 대한 공력해석을 수행하였다. 전진익 소형 항공기는 주익의 평면형상이 후퇴각을 가진 스트레이크(strake) 형태의 안쪽(inboard) 날개와, 전진각을 가진 바깥쪽(outboard) 날개가 결합되어 있는 형태로 구성되어 있다. 이와 같은 두개의 다른 형태의 날개 평면형상의 결합으로 킹크(kink)로 정의되는 날개의 불연속선이 존재하게 되어, 이 부분에 의한 날개 공력특성의 면밀한 분석이 요구되었다. 전진익 소형 항공기에 대한 기본적 공력계수의 산출 및 유동해석은 해석방법 간의 차이에서 기인하는 정확도를 분석하기 위해 4가지의 방법으로 계산을 수행하였다. 항공기 형상에 대한 격자생성의 용이성을 위해 중첩격자기법(Chimera grid)을 적용하였다. 본 해석을 통하여 전진익 소형기 형상에 대한 기본적인 공력계수의 도출과 함께 주익에 대한 공력특성이 분석되었다.

• 한국해양공학회:학술대회논문집
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• 한국해양공학회 2000년도 춘계학술대회 논문집
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• pp.23-28
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• 2000

The Green integral equation for the calculation of the forward-speed time-harmonic radiation-diffraction potentials IS derived. The forward-speed Green function presented by Brard is used and the correct free surface boundary condition for the Green function is imposed. The cause of the mistakes in the existing Green integral equation is also pointed out.

• 한국정밀공학회지
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• 제8권3호
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• pp.93-104
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• 1991

Limit analysis is based on the duality theorem which equates the least upper bound to the greatest lower bound. In this study, limit analysis of axisymmetric forming problem with workhardening materials is formulated by minimizing the upper bound functional and finite element program is developed for forward estrusion. Limit loads, velocity and flow line fields are directly obtained under various process conditions and deformation characteristics such as strains, strain rates and grid distortion are obtained from the optimum velocity components by numerical calculation. The experimental observation was carried out for extrusion and compared with computed results. The good agreement between theoretical and experimental results is shown that the developed programming is very effective for the analysis of axisymmetric extrusion.

• 전력전자학회논문지
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• 제6권5호
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• pp.453-459
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• 2001

본 논문에서는 Two-transistor 포워드 컨버터에서 사용 가능한 기존의 소프트 스위칭 기법과 새로운 소프트 스위칭 기법의 손실 분석을 수행한다. 두 트랜지스터에서 발생하는 스너버 전류에 의한 트랜지스터 손실과 내부 커패시터에 의한 턴-온 손실을 유도하고, 각각의 트랜지스터에서 발생하는 전체 손실을 계산한다. 손실 계산을 통해 기존의 소프트 스위칭 기법에서는 두 트랜지스터에서 발생하는 손실이 상이함을 보이고, 새로운 소프트 스위칭 기법에서는 손실이 적으면서도 두 트랜지스터에서의 손실이 고르게 발생함을 알 수 있다. 그리하여 제안된 소프트 스위칭 스너버를 사용하여 고른 열분포와 향상된 신뢰도를 얻을 수 있음을 보인다.

• 한국광학회지
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• 제14권4호
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• pp.460-465
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• 2003

Double-pass forward(DPF) 방식으로 구성되고 0.98 $\mu$m 파장 대역으로 펌핑된 자이로스코프용 erbium 첨가 광섬유(EDF) 광원의 출력광 특성을 수치계산을 이용하여 분석하였다. EDF길이, 펌프 power, 그리고 펌프 파장 등의 변화에 따른 출력광 power, 파장선폭, 중심파장 안정성 둥을 분석하였으며 일부 특성에 대하여 실험결과와 비교ㆍ검증하였다. 그 결과, DPF 방식의 EDF 광원에서 광원의 특성이 EDF 길이에 크게 의존함을 알 수 있었으며 펌프 power와 펌프 파장의 변화에 대해서 안정된 중심파장을 얻을 수 있는 최적 동작조건도 존재함을 알 수 있었다.

• 한국소음진동공학회논문집
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• 제12권3호
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• pp.213-220
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• 2002

Modifying effects of the rectangular forward step for suppressing the unsteady pressure fluctuation during interaction between the upstream vortical flow and the edge are studied numerically. The vertical flow is modeled by a point vortex, and the unsteady pressure coefficient is obtained from the velocity and the potential fields. To investigate the effects of the edge shape the rectangular forward step is chamfered wish various angles. Calculation shows that the pressure peaks become decreased by increasing the vortex height as well as the chamfering angle. The pressure amplitudes are very sensitive to the change of the initial vertex height and its strength. From this study we can find out that the chamfered edge has two effects; the one is that it suppresses the pressure amplitude generated from the edge, and the other is that it decreases the time variation of unsteady pressure fluctuation. These modifying concepts can be applied to attenuate the self-sustained oscillation mechanism at the open cavity flow.