• Title/Summary/Keyword: Captured wave ratio

검색결과 12건 처리시간 0.025초

근사기법을 활용한 공진형 파력발전 부이의 발전량 추정 및 최적설계 (Power Estimation and Optimum Design of a Buoy for the Resonant Type Wave Energy Converter Using Approximation Scheme)

  • 고혁준;유원선;조일형
    • 한국해양공학회지
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    • 제27권1호
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    • pp.85-92
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    • 2013
  • This paper deals with the resonant type of a WEC (wave energy converter) and the determination method of its geometric parameters which were obtained to construct the robust and optimal structure, respectively. In detail, the optimization problem is formulated with the constraints composed of the response surfaces which stand for the resonance period(heave, pitch) and the meta center height of the buoy. Use of a signal-to-noise ratio calculated from normalized multi-objective results with the weight factor can help to select the robust design level. In order to get the sample data set, the motion responses of the power buoy were analyzed using the BEM (boundary element method)-based commercial code. Also, the optimization result is compared with a robust design for a feasibility study. Finally, the power efficiency of the WEC with the optimum design variables is estimated as the captured wave ratio resulting from absorbed power which mainly related to PTO (power take off) damping. It could be said that the resultant of the WEC design is the economical optimal design which satisfy the given constraints.

연료-공기 비혼합도가 희박예혼합 연소 특성에 미치는 영향 (Effects of Fuel-Air Unmixedness on Lean Premixed Combustion Characteristics)

  • 김대현;이종호;전충환;장영준
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2002년도 제24회 KOSCO SYMPOSIUM 논문집
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    • pp.133-139
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    • 2002
  • The lean premixed technique has been proven very efficient in reducing NOx emissions from gas turbine combustors. However combustion instability is susceptible to occur in lean premixed combustor. So laboratory-scale dump combustor was used to understanding the underlying mechanisms causing combustion instabilities. In this study, tests were conducted at atmospheric pressure and inlet air was up to $360^{\circ}C$ with natural gas. The observed instability was a longitudinal mode with a frequency of ${\sim}341.8Hz$. At selected unstable conditions, phase-resolved OH chemiluminescence images were captured to investigate flame structure with various equivalence ratio. Combustion instability was observed to occur at higher value of equivalence ratio(>0.69). This study was performed to investigate the effects of equivalence ratio and fuel split measuring NOx and acoustic wave. The results reveal the effect of fuel-air unmixedness on lean premixed combustor.

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정상초음파의 교란을 받는 메탄-공기 예혼합화염의 전파특성에 대한 초음파 구동 주파수의 영향 (Effects of Driving Frequency on Propagation Characteristics of Methane-Air Premixed Flame Influenced by Ultrasonic Standing Wave)

  • 배대석;서항석;김정수
    • 대한기계학회논문집B
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    • 제39권2호
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    • pp.161-168
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    • 2015
  • 정상초음파장의 구동 주파수가 메탄-공기 예혼합화염의 전파특성에 미치는 영향을 규명하고자 하는 실험결과를 제시한다. 고속카메라를 이용하여 화염의 전파영상을 획득하였으며, 영상 후처리를 통해 화염선단의 구조와 속도변이를 포함하는 화염의 거시적 거동을 상세히 관찰하였다. 정상초음파가 연소반응을 촉진시켜 화염 전파속도의 증대와 화염선단 구조의 변이를 유발한다는 사실에 더하여, 초음파구동 주파수와 당량비에 대한 화염거동의 종속성을 확인하였다.

Passive Millimeter-Wave Image Deblurring Using Adaptively Accelerated Maximum Entropy Method

  • Singh, Manoj Kumar;Kim, Sung-Hyun;Kim, Yong-Hoon;Tiwary, U.S.
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 2007년도 Proceedings of ISRS 2007
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    • pp.414-417
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    • 2007
  • In this paper we present an adaptive method for accelerating conventional Maximum Entropy Method (MEM) for restoration of Passive Millimeter-Wave (PMMW) image from its blurred and noisy version. MEM is nonlinear and its convergence is very slow. We present a new method to accelerate the MEM by using an exponent on the correction ratio. In this method the exponent is computed adaptively in each iteration, using first-order derivatives of deblurred image in previous two iterations. Using this exponent the accelerated MEM emphasizes speed at the beginning stages and stability at later stages. In accelerated MEM the non-negativity is automatically ensured and also conservation of flux without additional computation. Simulation study shows that the accelerated MEM gives better results in terms of RMSE, SNR, moreover, it takes only about 46% lesser iterations than conventional MEM. This is also confirmed by applying this algorithm on actual PMMW image captured by 94 GHz mechanically scanned radiometer.

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비정렬 격자에서 Ghost Fluid 법을 이용한 밀도약층 주위 수중운동체에 의한 유동 해석 (NUMERICAL ANALYSIS OF FLOW AROUND A SUBMERGED BODY NEAR A PYCNOCLINE USING THE GHOST FLUID METHOD ON UNSTRUCTURED GRIDS)

  • 신상묵
    • 한국전산유체공학회지
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    • 제10권3호
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    • pp.70-76
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    • 2005
  • A two-layer incompressible time-accurate Euler solver is applied to analyze flow fields around a submerged body moving at a critical speed near a pycnocline. Discontinuities in the dependent variables across the material interface are captured without any dissipation or oscillation using the ghost fluid method on an unstructured grid. It is shown that the material interlace has significant effects on forces acting on a submerged body moving near a pycnocline regardless of the small difference in densities of two layers. Contrary to the shallow water waves, a submerged body can reach a critical speed at very low Froude number due to the small difference in the densities of the two layers.

모형 가스터빈 연소기내 연소불안정성에 대한 실험적 연구 (An Experimental Study on Combustion Instability Mechanism in a Dump Gas Turbine Combustor)

  • 이연주;이종호;전충환;장영준
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 추계학술대회논문집B
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    • pp.853-858
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    • 2001
  • The knowledge of flame structure is essential for control of combustion instability phenomena. Some results of an experimental study on mechanism of naturally occurring combustion oscillations with a single dominant frequency are presented. Tests were conducted in a laboratory-scale dump combustor at atmospheric pressure. Sound level meter was used to track the pressure wave inside the combustor. The observed instability was a longitudinal mode with a frequency of $\sim341.8Hz$. Instability map was obtained at the condition of inlet temperature of $360^{\circ}C$, mean velocities of $8.5\sim10.8m/s$ and well premixed mixture. It showed that combustion instability was susceptible to occur in the lean conditions. In this study, unstable flame was observed from stoichiometric to 0.7 in overall equivalence ratio. At selected unstable conditions, phase-resolved OH chemiluminescence images were captured to investigate flame structure with various mean velocities. As mean velocity is increased, the flame grows and global heat release was changed. Due to these effects, combustion instability can be maintained at more lean air-fuel ratio. Also, these results give an insight to the controlling mechanism for an increasing heat release at maximum pressure.

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박스형 모델에 의한 슬로싱 하중에 관한 실험적 연구 (An Experimental Study on Rectangular Box Sloshing)

  • 정동우;전수성;박준수;권순홍;장택수
    • 한국해양공학회:학술대회논문집
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    • 한국해양공학회 2006년 창립20주년기념 정기학술대회 및 국제워크샵
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    • pp.386-391
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    • 2006
  • This study presents experimental results of sloshing phenomenon done on rectangular box. A simple harmonic excitation was done on the box. Two kinds of filling ratio, 20% and 30% of height, were tested. A total of 15 pressure sensors were installed to monitor the impact pressure. Each test was repeated for 20 times to ensure the repeatability. The high speed camera captured the flaw filed and the corresponding pressure were synchronize with video signal so that the video image can help the interpretation of the impact pressure. The two filling ratio made difference in the flaw characteristic and impact pressure. The use of high speed camera made it possible to understand the bubble generation mechanism. The pressure time histories were presented.

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3차원 차분격자볼츠만 모델에의 내부자유도 적용 및 유동소음 모사 (Application of the Internal Degree of Freedom to 3D FDLB Model and Simulations of Aero-Acoustic)

  • 강호근;안수환;김정환
    • 대한조선학회논문집
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    • 제43권5호
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    • pp.586-596
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    • 2006
  • A 3-dimensional FDLB model with additional internal degree of freedom is applied for diatomic gases such as air, in which an additional distribution function is introduced. Direct simulations of aero-acoustic by using the applied model and scheme are presented. Speed of sound is correctly recovered. As typical examples, the Aeolian tone emitted by a circular column is successfully simulated even very low Mach number flow. Acoustic pressure fluctuations with the same frequency of the Karman vortex street compared with the pressure fluctuation around a circular column is captured. Full three-dimensional acoustic wave past a compact block like pentagon, furthermore, is also emitted in y direction as dipole like sound.

Ultrasonic Evaluation of Interfacial Stiffness for Nonlinear Contact Surfaces

  • Kim, Noh-Yu;Kim, Hyun-Dong;Cho, Youn-Ho
    • 비파괴검사학회지
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    • 제28권6호
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    • pp.504-511
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    • 2008
  • This paper proposes an ultrasonic measurement method for measurement of linear interfacial stiffness of contacting surface between two steel plates subjected to nominal compression pressures. Interfacial stiffness was evaluated by using shear waves reflected at contact interface of two identical solid plates. Three consecutive reflection waves from solid-solid surface are captured by pulse-echo method to evaluate the state of contact interface. A non-dimensional parameter defined as the ratio of their peak-to-peak amplitudes are formulated and used to calculate the quantitative stiffness of interface. Mathematical model for 1-D wave propagation across interfaces is developed to formulate the reflection and transmission waves across the interface and to determine the interfacial stiffness. Two identical plates are fabricated and assembled to form contacting surface and to measure interfacial stiffness at different states of contact pressure by means of bolt fastening. It is found from experiment that the amplitude of interfacial stiffness is dependent on the pressure and successfully determined by employing pulse-echo ultrasonic method without measuring through-transmission waves.

PECVD에 의한 Sirich 산화막의 특성 (Characteristics of Silicon Rich Oxide by PECVD)

  • 강선화;이상규;박홍락;고철기;최수한
    • 한국재료학회지
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    • 제3권5호
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    • pp.459-465
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    • 1993
  • SOG박막 밑에 층간 절연박으로 사용하는 PECVD산화막을 Si rich산화막으로 만들어 줌으로써 실리콘 dangling bond가 수소원자나 수분과 결합하여 SOG박막으로 부터 침투되는 수소원자나 수분의 확산을 억제하므로서 소작 열화되는 것을 방지한다. 이러한 Si rich산화막의 기본 특성을 알아보기 위하여 LF/HF power비와 $SiH_4/N_2O$ gas유량비를 변화시켜서 박막 특성을 조사하였다. 저주파 power만 변화시킨 경우, 증착속도가 감소하고 굴절율과 압축응력에 증가하며 FTIR에서 3300$\textrm{cm}^{-1}$~3800$\textrm{cm}^{-1}$영역의 수분에 의한 peak이 감소하는 것으로 보아 박막이 치밀해짐을 알 수 있고, $SiH_{4}$기체유량을 증가시킨 경우엔 증착속도, 굴절율, 식각속도는 증가하나 압축응력은 감소한다. FTIR에서 Si-O-Si peak의 세기가 감소하고 낮은 파수영역으로 이동하며, AES분석 결과에서 일반적인 oxide(Si:0=1:1.98)에서 보다 Si:O비가 1:1.23으로 낮아 PECVD산화 막내의 Si danling bond가 증가했음을 알 수 있었다.

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