• 한국전산구조공학회논문집
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• 제33권1호
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• pp.1-7
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• 2020

트윈 빌딩의 풍응답은 풍하중의 공력 특성과 트윈 빌딩 구조 시스템의 동적 특성에 영향을 받는다. 본 논문에서는 트윈 빌딩의 두 빌딩의 간격이 다른 두 경우에 대해서 풍응답에 영향을 주는 풍압의 특성을 풍동 실험과 적합 직교 분해 기법을 이용해 파악하고, 3차원 구조 시스템 모델링을 통해 동특성을 파악하였다. 그리고 이중 모달 변환 기법을 이용해서 각 풍압의 특성과 구조물의 동특성이 풍응답에 미치는 영향을 파악하였다. 적합 직교 분해 기법을 통해서 채널링과 와류 효과에 대해서 파악할 수 있었다. 풍 직각 방향의 풍하중은 두 빌딩의 간격에 영향을 많이 받았으며, 풍 방향의 풍하중은 간격에 영향을 적게 받았다. 마찬가지로, 이중 모달 변환 기법에서 교차 참여 계수는 풍 직각 방향에서는 두 빌딩의 간격에 따라 크게 달라진 반면, 풍 방향은 영향이 적었다. 이에 따라 두 빌딩의 간격이 풍 방향의 풍응답 보다 풍 직각 뱡향의 풍응답에 중요한 역할을 하는 것을 알 수 있었다.

• International Journal of Aeronautical and Space Sciences
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• 제14권3호
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• pp.229-236
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• 2013

This paper presents the experimental investigation of a biplane micro air vehicle. The effects of geometric parameters, gap, stagger, and decalage angle are investigated at low Reynolds number (~150,000) in a low-speed wind tunnel. A rigid flat plate with an aspect ratio of one and square planform shape is used to evaluate all three geometric parameters. The side dimension of the single flat plate is 0.15 m. The goal is to find an optimal biplane configuration that should exceed monoplane performance by generating high lift and flying as slow as possible, in order to capture high-quality visual recordings. This configuration will directly help to fly at a lower velocity and to make tighter turns that are advantageous in restricted environments. The results show that the aerodynamic performance of the biplane MAV is significantly enhanced through the combination of gap and stagger effects. A performance comparison demonstrates the superiority of the optimal biplane configuration compared to a monoplane in cruise and glide phases. Moreover, no significant compromise is found for the range, endurance, and climb performance.

• Wind and Structures
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• 제35권3호
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• pp.177-191
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• 2022

Trains emerging on a streamlined bridge-girder may have salient interference effects on the aerodynamic properties of the bridge. The present paper aims at investigating these interferences by wind tunnel measurements, covering surface pressure distributions, near wake profiles, and flow visualizations. Experimental results show that the above interferences can be categorized into two primary effects, i.e., an additional angle of attack (AoA) and an enhancement in flow separation. The additional AoA effect is demonstrated by the upward-moved stagnation point of the oncoming flow, the up-shifted global symmetrical axis of flow around the bridge-girder, and the clockwise-deflected orientation of flow approaching the bridge-girder. Due to this additional AoA effect, the two critical AoAs, where flow around the bridge-girder transits from trailing-edge vortex shedding (TEVS) to impinging leading-edge vortices (ILEV) and from ILEV to leading-edge vortex shedding (LEVS) of the bridge-girder are increased by 4° with respect to the same bridge-girder without trains. On the other hand, the underlying flow physics of the enhancement in flow separation is the large-scale vortices shedding from trains instead of TEVS, ILEV, and LEVS governed the upper half bridge-girder without trains in different ranges of AoA. Because of this enhancement, the mean lift and moment force coefficients, all the three fluctuating force coefficients (drag, lift, and moment), and the aerodynamic span-wise correlation of the bridge-girder are more significant than those without trains.

• International Journal of Aeronautical and Space Sciences
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• 제11권3호
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• pp.175-183
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• 2010

The increased demand for a higher performing magnetic suspension and balance system (MSBS) resulted in an increase in costs for the efforts necessary for achieving an improved MSBS. Therefore, MSBS performance should be predicted during the design in order to reduce risk. This paper presents the modeling and simulation of an MSBS that controls 6-degree of freedom (DOF) of an aerodynamic body within the MSBS. Permanent magnets and electromagnets were modeled as coils, and this assumption was verified by experimental results. Finally, an MSBS simulator was developed, predicting that the MSBS is able to contain the model within a bounded region as well as measure external forces acting on the body during wind tunnel tests.

• 한국전산구조공학회논문집
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• 제13권4호
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• pp.405-415
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• 2000

한 구조물에 작용하는 풍압력 시계열이 자기회귀 이동평균(ARMA) 모델을 사용하여 모델화 된다. AR 과정에서 시계열의 현재 값은 유한한 수의 이전 값들의 선형적 결합과 한 백색잡음에 의해 나타난다. MA 과정에서 시계열의 현재값은 유한한 수의 이전 백색잡음들에 선형적이다. ARMA 과정은 AR과 MA 과정의 결합이다. 본 논문에서, AR, MA와 ARMA 모델이 풍압력 시계열에 적용되고, 데이터를 나타내기에 가장 적합한 ARMA 모델을 선정하는 과정이 소개된다. 모델의 변수들은 최대 가능도법을 사용하여 산정되고, 압력 시계열의 시간적 복잡성의 척도인 모델 차수를 최적화하기 위해 AICC 모델 선정 기준이 사용된다. 또한, 모델의 유효성을 조사하기 위해 LBP 검사가 사용된다. 본 연구로부터, AR 과정이 풍압력 시계열을 나타내기에 가장 적합하다는 결론이 얻어진다.

• 자원환경지질
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• 제31권6호
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• pp.535-545
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• 1998

Various geophysical methods have been applied to the survey of the lava tunnel of Manjanggul in Cheju Island to study the effectiveness of each method in investigating underground tunnels. The surveys employing gravity, magnetic, electrical, AMT and VLF methods were carried out along seven profiles across the Manjanggul; especially, all the five methods were used on one representative profile. Several aspects of different methods pertinent to their use in investigation of underground tunnels have been noted. The electrical method employing the dipole-dipole array appeared to be the most effective one among five methods. Therefore, we have tested the electrical method more carefully by using various electrode spacings, and obtained successful resistivity sections showing the existence of lava tunnels. The gravity method provided relatively successful responses associated with the tunnel although the gravity readings were contaminated by wind blowing during the survey. The gravity data were also useful for the quantitative modeling study. The magnetic data were also successful in delineating the tunnel qualitatively. The AMT data were not successful because the used frequency band was not appropriate in detecting very shallow target. The VLF data were severely influenced by the neighboring noise sources such as power lines and were not successful in detecting the tunnel responses. The comprehensive result of electrical, gravity and magnetic surveys suggests that undiscovered lava tunnels may exist adjacent to the Manjanggul.

• 환경영향평가
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• 제9권1호
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• pp.61-74
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• 2000

This study compares the results of environmental impact assessment with the results of post-environmental investigation, using the case of Taean thermal power plant construction. The atmospheric and water qualities were not greatly changed before and after the construction of the power plant. However, the site of the highest concentration predicted by the atmospheric quality modeling in environmental impact assessment was different from that after operation of 4 power plants. There was also a difference in the diffusion range of thermal discharge water between the measured result(1km) and the predicted value(1.5km) with the model. Thus, environmental impact evaluation should be based on long-term (more than a year) environmental monitoring data. For the modeling of atmospheric quality and numerical thermal discharge water diffusion, appropriate models for each plant should be selected and the numerical modeling should be accompanied by computer simulation, wind tunnel test, etc. Moreover, environmental evaluation should focus more on the degree of impact on surroundings than the prediction of changes in surroundings caused by operation of plants.

• 한국항공우주학회지
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• 제40권8호
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• pp.647-654
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• 2012

외부 환경조건에 의한 항공기 위협인자로서 과냉각 대형 액적은 그 중요성이 지속적으로 보고되고 있다. 이러한 대형 액적의 거동은 상대적으로 작은 액적과 달리 그 형태가 변화하며 액적이 표면과 충돌시 파편이 발생하는 등 다양한 물리적 특성을 나타낸다. 이러한 대형 액적의 거동을 시뮬레이션 하기 위해 비정렬 격자계 기반 2차원 압축성 Navier-Stokes 코드와 액적 거동 시뮬레이션 코드를 개발하였다. 또한 대형 액적의 물리적 현상을 모사하기 위해 반경험적 기법에 기반한 액적항력모델과 액적-고체표면 충돌 모델을 기존 액적장 지배방정식의 액적항력계수 및 경계면의 수치적 경계조건으로 적용하였다. 그 결과 풍동 시험과 액적충돌 영역 및 최대 축적율은 매우 유사하게 나타난 반면 NACA23012 익형의 아랫면 주위 축적율의 경향은 풍동 시험보다 다소 크게 나타났다.

• 한국항공우주학회지
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• 제44권6호
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• pp.537-543
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• 2016

KF-16의 1/33 축소 모형 공력 데이터베이스를 기반으로 풍동실험에 적응적 실험설계법을 적용하는 경우 실험의 정확도뿐만 아니라 풍동 실험에 소요되는 비용을 최소화할 수 있도록 추가 실험점 선택 방법에 대한 연구를 수행하였다. 라틴방격법을 이용하여 초기실험점을 선택하였고, Gaussian Process를 통해 불확실성이 가장 크면서도 실험에 소요되는 비용이 상대적으로 적은 추가 실험점을 선택하였다. 공력계수 모델링은 가장 비선형성이 큰 피칭모멘트계수를 정확히 모델링 하는 것을 목표로 하였다. 실험 비용을 고려한 적응적 실험설계법을 적용한 경우, 기존의 적응적 실험설계 방법론에 비해 모델의 정확도와 실험에 소요되는 비용에 어떤 영향을 미치는지 알아보았다.

• Wind and Structures
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• 제32권4호
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• pp.309-319
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• 2021

The vortex-drift pattern over a girder surface, actually demonstrating the complex fluid-structure interactions between the structure and surrounding flow, is strongly correlated with the VIVs but has still not been elucidated and may be useful for modeling VIVs. The complex fluid-structure interactions between the structure and surrounding flow are considerably simplified in constructing a vortex model to describe the vortex-drift pattern characterized by the ratio of the vortex-drift velocity to the oncoming flow velocity, considering the aerodynamic work. A spring-suspended sectional model (SSSM) is used to measure the pressure in wind tunnel tests, and the aerodynamic parameters for a typical streamlined closed-box girder are obtained from the spatial distribution of the phase lags between the distributed aerodynamic forces at each pressure point and the vortex-excited forces (VEFs). The results show that the ratio of the vortex-drift velocity to the oncoming flow velocity is inversely proportional to the vibration amplitude in the lock-in region and therefore attributed to the "lock-in" phenomena of the VIVs. Installing spoilers on handrails can destroy the regular vortex-drift pattern along the girder surface and thus suppress vertical VIVs.