• International Journal of Aeronautical and Space Sciences
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• 제18권1호
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• pp.165-173
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• 2017

The aeromechanics predictions of HART I rotor obtained using a computational structural dynamics (CSD) code are evaluated against the wind tunnel test data. The flight regimes include low speed descending flight at an advance ratio of ${\mu}=0.151$ and cruise condition at ${\mu}=0.229$. A lifting-line based unsteady airfoil theory with C81 table look-up is used to calculate the aerodynamic loads acting on the blade. Either rolled-up free wake or multiple-trailer wake with consolidation (MTC) model is employed for the free vortex wake representation. The measured blade properties accomplished recently are used to analyze the rotor for the up-to-date computations. The comparison results on airloads and structural loads of the rotor show good agreements for descent flight and fair for cruise flight condition. It is observed that MTC model generally improves the correlation against the measured data. The structural loads predictions for all measurement locations of HART I rotor are investigated. The dominant harmonic response of the structural loads is clearly captured with MTC model.

• 한국정보과학회:학술대회논문집
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• 한국정보과학회 2010년도 한국컴퓨터종합학술대회논문집 Vol.37 No.1(D)
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• pp.360-365
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• 2010

In this paper, we present a distributed algorithm for detecting dynamic event regions in wireless sensor network with the consideration on energy saving. Our model is that the sensing field is monitored by a large number of randomly distributed sensors with low-power battery and limited functionality, and that the event region is dynamic with motion or changing the shape. At any time that the event happens, we need some sensors awake to detect it and to wake up its k-hop neighbors to detect further events. Scheduling for the network to save the total power-cost or to maximize the monitoring time has been studied extensively. Our scheme is that some predetermined sensors, called critical sensors are awake all the time and when the event is detected by a critical sensor the sensor broadcasts to the neighbors to check their sensing area. Then the neighbors check their area and decide whether they wake up or remain in sleeping mode with certain criteria. Our algorithm uses only 2 bit of information in communication between sensors, thus the total communication cost is low, and the speed of detecting all event region is high. We adapt two kinds of measure for the wake-up decision. With suitable threshold values, our algorithm can be applied for many applications and for the trade-off between energy saving and the efficiency of event detection.

• 한국통신학회논문지
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• 제32권12A호
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• pp.1303-1310
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• 2007

IEEE 802.11b 무선 네트워크에서 스테이션들이 저전력 모드로 동작할 때, 스테이션들은 액세스 포인트 (AP)가 주기적으로 전송하는 비콘(beacon)을 수신하여 동기를 맞춘다. 예정된 시각에 무선채널이 사용 중인 경우 AP에서 비콘 전송이 지연되므로, 스테이션은 비콘을 수신하기 위해 충분한 시간 동안 깨어있어야 한다. 이 논문에서는 수신된 비콘의 지연시간을 측정하여 다음 비콘을 수신하기 위해 스테이션이 깨어있어야 할 시간을 결정하는 방법을 제안한다. AP에서 비콘의 전송지연에 대해 분석하였다. 제안된 방법에 대해 모의실험이 수행되었고 분석을 통해 제안된 방법의 특성을 설명하였다. 스테이션이 깨어있는 시간으로 측정된 결과는 에너지 소모가 개선될 수 있음을 보여준다.

• 한국음향학회지
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• 제39권5호
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• pp.468-475
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• 2020

단어의 특성을 잘 표현하는 음성 단어 임베딩은 기동어 인식에서 중요한 역할을 한다. 하지만 기동어 인식이 수행되는 환경에서 필연적으로 발생하는 다양한 종류의 잡음으로 인해 음성 단어 임베딩의 표현 능력이 손상될 수 있으며, 인식 성능의 저하를 초래할 수 있다. 본 논문에서는 음성 단어 임베딩에 영향을 줄 수 있는 환경적인 요인을 완화시키는 삼중항 손실 기반의 도메인 적대적 훈련 방식을 제안한다. 잡음 환경에서의 기동어 검출 실험을 통해 제안하는 방식이 기존의 도메인 적대적 훈련 방식을 효과적으로 개선하는 모습을 확인할 수 있었고, 잡음 환경에서의 기동어 검출을 위해 기존에 제안된 다른 방법과의 결합을 통해 제안하는 방식의 확장성을 확인할 수 있었다.

• 한국가시화정보학회:학술대회논문집
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• 한국가시화정보학회 2005년도 추계학술대회 논문집
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• pp.50-53
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• 2005

The turbulent flow around a sphere was investigated in a streamwise meridian plane using two experimental techniques: smoke-wire flow visualization in wind tunnel at Re=5,300 and PIV measurements in a circulating water channel at Re=7,400. The smoke-wire visualization shows flow separation points near an azimuthal angle of $90^{\circ}$, recirculating flow, transition from laminar to turbulent shear layer, evolving vortex roll-up and fully turbulent eddies in the sphere wake. In addition, the mean flow pattern extracted by particle tracing method in water tunnel at Re= 14,500 reveals two distinct comparable toroidal(not closed) vortices in the recirculation region. The mean velocity field measured using a PIV technique demonstrates the detailed wake configuration of close symmetric recirculation and near-wake configuration with two toroidal vortices, reversed velocity zone and vorticity contours.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 추계학술대회
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• pp.950-955
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• 2003

The fluid propulsion mechanism of two oscillating flat plates is studied numerically using a discrete vortex method. Presently, the flat plates are assumed to be rigid. To analyze the closely coupled aerodynamic interference between the flat plates, a core addition scheme and a vortex core model are combined together. A calculated wake pattern for a flat plate in heaving oscillation motion is compared with the flow visualization. The effect of wake shapes on the aerodynamic characteristics of the flat plate in pitching oscillation is investigated. The velocity profiles behind the flat plates in pitching oscillations are plotted to investigate the possible thrust generation mechanism.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2004년도 춘계학술대회
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• pp.1720-1725
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• 2004

The present study addresses a computational work to investigate the influence of a turbulent wake flow on the pressure recovery of a two-dimensional subsonic diffuser. The turbulent wake is generated by a cylinder with a small diameter, which is installed at the diffuser inlet. Computation is applied to two-dimensional steady Navier-Stokes equations. The computational results are qualitatively well compared to existing experimental data. The results show that the diffuser pressure recovery is strongly dependent on the diameter and location of the cylinder. It is found that there is a certain diameter and location of cylinder for the diffuser pressure recovery to be most enhanced. Compared with no cylinder case, the diffuser performance increases up 24%.

• 한국음향학회지
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• 제39권2호
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• pp.131-136
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• 2020

음성 인식기를 대기모드에서 동작 모드로 전환하기 위해 발화하는 짧은 단어를 기동어(Wake Up Word, WUW)라고 하며, 음성 인식기를 실제로 사용하는 사용자가 지정한 기동어를 사용자 정의 기동어라고 한다. 본 논문에서는 이러한 사용자 정의 기동어를 인식하기 위해 기존의 Gaussian Mixture Model-Hidden Markov Model(GMM-HMM) 기반의 시스템, Linear Discriminant Analysis(LDA)를 적용한 LDA-GMM-HMM 기반의 시스템과, LDA-GMM-HMM 모델에서 GMM을 Deep Neural Network(DNN)로 대체한 LDA-DNN-HMM 기반의 시스템을 제작하고 각 시스템의 사용자 정의 기동어 인식 성능 및 비기동어 거절 성능을 비교한다. 또한 기동어 인식기의 체감 성능을 향상시키고자 각 모델에 threshold를 적용하여 기동어 인식 실패율을 약 10 % 수준으로 감소 시킨 후에 비기동어(non-WUW)의 거절 실패율을 비교 평가한다. Threshold 적용시에 LDA-DNN-HMM 기반의 시스템의 경우 기동어 인식 실패율 9.84 % 수준에서 비기동어 거절 실패율이 0.0058 %의 인식 성능을 나타내어 LDA-GMM-HMM 시스템 보다 약 4.82배 향상된 비기동어 거절 성능을 나타낸다. 이러한 결과는 본 논문에서 제작한 LDA-DNN-HMM 모델이 사용자 정의 기동어 인식 시스템을 구축하는데 효과적임을 입증한다.

• 한국해양공학회지
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• 제33권1호
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• pp.26-32
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• 2019

The vortex flow behind a bluff body has been a subject of interest for a very long time because of its engineering applicability such as to vortex induced vibration. In the near wake of a bluff body, vortices are periodically shed in two shear layers, which originate in the trailing edges. The far wake is made up of the classical Karman vortices, which are connected together by streamwise and spanwise vortices. These vortex formations have been studied in many experimental and numerical ways. However, most of the studies considered non-cavitating flow. In this study, we investigated cavitating flow in the wake of a two-dimensional wedge. Experiments were conducted in a cavitation tunnel of Chungnam National University. Using a particle image velocimetry (PIV), we measured the velocity fields under two different flow conditions: non-cavitating and cavitating regimes. We also investigated the vortex shedding frequencies using an absolute pressure transducer mounted on the top of the test window. Throughout the experiments, it was found that the shedding frequency of the vortex was strongly affected by cavitation, and the Strouhal number could exceed its value in the non-cavitating regime.

• Wind and Structures
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• 제29권2호
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• pp.139-147
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• 2019

One of the most important factors in tall buildings design in urban spaces is wind. The present study aims to investigate the aerodynamic behavior in the square and triangular footprint forms through aerodynamic modifications including rounded corners, chamfered corners and recessed corners in order to reduce the length of tall buildings wake region. The method used was similar to wind tunnel numerical simulation conducted on 16 building models through Autodesk Flow Design 2014 software. The findings revealed that in order to design tall 50 story buildings with a height of about 150 meters, the model in triangular footprint with aerodynamic modification of chamfered corner facing wind direction came out to have the best aerodynamic behavior comparing the other models. In comparison to the related reference model (i.e., the triangular footprint with sharp corners and no aerodynamic modification), it could reduce the length of the wake region about 50% in general. Also, the model with square footprint and aerodynamic modification of chamfered corner with the corner facing the wind could present favorable aerodynamic behavior comparing the other models of the same cluster. In comparison to the related reference model (i.e., the square footprint with sharp corners and no aerodynamic modification), it could decrease the wake region up to 30% lengthwise.