• Title/Summary/Keyword: CCM type

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대형 비행갑판을 갖는 함정과 풍동시험 결과를 활용한 고신뢰도 함정 Airwake 예측 (High-Fidelity Ship Airwake CFD Simulation Method Using Actual Large Ship Measurement and Wind Tunnel Test Results )

  • 정진덕;조태환;이승훈;최재훈;이학민
    • 대한조선학회논문집
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    • 제60권2호
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    • pp.135-145
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    • 2023
  • Developing high-fidelity Computational Fluid Dynamics (CFD) simulation methods used to evaluate the airwake characteristics along a flight deck of a large ship, the various kind of data such as actual ship measurement and wind tunnel results are required to verify the accuracy of CFD simulation. Inflow velocity profile at the bow, local unsteady flow field data around the flight deck, and highly reliable wind tunnel data which were measured after reviewing Atmospheric Boundary Layer (ABL) simulation and Reynolds Number effects were also used to determine the key parameters such as turbulence model, time resolution and accuracy, grid resolution and type, inflow condition, domain size, simulation length, and so on in STAR CCM+. Velocity ratio and turbulent intensity difference between Full-scale CFD and actual ship measurement at the measurement points show less than 2% and 1.7% respectively. And differences in velocity ratio and turbulence intensity between wind tunnel test and small-scale CFD are both less than 2.2%. Based upon this fact, the selected parameters in CFD simulation are highly reliable for a specific wind condition.

CFD 해석을 통한 냉장고용 응축기 전열성능 연구 (CFD ANALYSIS OF HEAT TRANSFER PERFORMANCE OF A REFRIGERATOR CONDENSER)

  • 유성수;황도연;이명수;한병윤;박형구
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2009년 춘계학술대회논문집
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    • pp.303-309
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    • 2009
  • In this study, the heat transfer and flow field of condenser used on Kim-chi refrigerator is analysed with numerical method. Main objective is to present the base data for designing new condenser model with improvement of heat transfer performance. For CFD analysis, a commercial code, STAR-CCM+ was used. The water was used for the inner working fluid and the air was used for the outer fluid. The condenser type used in this study is a flat plate fin-and-tube heat exchanger. As factors for performance analysis, the effect of condenser geometry and air velocity was investigated. As a result, it has been observed that there is a suitable fin pitch with which heat transfer performance of condenser is maximized.

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DSP를 이용한 부스트 컨버터의 전류 제어기 설계 및 구현 (Design and Implementation of a Current Controller for Boost Converters Using a DSP)

  • 이광운
    • 전력전자학회논문지
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    • 제17권3호
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    • pp.259-265
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    • 2012
  • This paper introduces a method for design and implementation of a current controller for boost converter operating in continuous conduction mode (CCM) using a digital signal processor (DSP). A Proportional-Integral (PI) type current controller outputs an average voltage command for inductor, used in the input side of the boost converter, and the duty-ratio of PWM (pulse width modulation) signal for switching device is directly calculated from the average voltage command. The gains of the PI current controller are selected such that the current response characteristics are the same as those of a first-order low-pass filter. The proposed current control scheme is implemented using a DSP based on fixed-point math operations and an experimental study has been performed to validate the proposed method.

Measurement Uncertainties for Vacuum Standards from a Low to an Ultra-high Vacuum

  • Hong, S.S.;Shin, Y.H.;Lim, J.Y.
    • Applied Science and Convergence Technology
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    • 제23권3호
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    • pp.103-112
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    • 2014
  • The Korea Research Institute of Standards and Science (KRISS) has three major vacuum systems: an ultrasonic interferometer manometer (UIM; Section II, Figs. 1 and 2) for a low vacuum, a static expansion system (SES; Section III, Figs. 3 and 4) for a medium vacuum, and an orifice-type dynamic expansion system (DES, Section IV, Figs. 5 and 6) for high and ultra-high vacuum systems. For each system, explicit measurement model equations with multiple variables are given. According to ISO standards, all of these system variable errors were used to calculate the expanded uncertainty (U). For each system, the expanded uncertainties (k = 1, confidence level = 95%) and relative expanded uncertainty (expanded uncertainty/generated pressure) levels are summarized in Table 4. Within the uncertainty limits, our bilateral and key comparisons [CCM.P-K4 (10 Pa to 1 kPa)] are extensive and in good agreement with those of other nations (Fig. 8 and Table 5).

PWM 제어를 이용한 고역율, 저교조파형 고출력 Sepic 컨버터에 관한 연구 (A study on the high-power Sepic converter for high-power-factor, low current harmonics using PWM control)

  • 주형종;권명일;장도현
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2003년도 하계학술대회 논문집 B
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    • pp.1211-1213
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    • 2003
  • A pulse width modulation(PWM) method for single-phase Sepic-type rectifier is introduced in this paper. The characteristics of the proposed PWM system are high performance high power factor with low input current harmonic distortion. The proposed control method is based on the average-current-mode using the dedicated integrated circuit UC3854 this technique it is possible to implement a very simple control circuit for unitary power-factor in CCM operation and also to provide over-current protection.

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디지털 제어를 이용한 Interleaving CRM 플라이백 타입 DC-AC 인버터의 구현 (Implementation of interleaved Critical mode Flyback type DC-AC inverter using digital controller)

  • 김지태;이규찬;서갑수;현병철;배현수;조보형
    • 전력전자학회:학술대회논문집
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    • 전력전자학회 2010년도 추계학술대회
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    • pp.13-14
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    • 2010
  • 본 논문에서는 경계 모드(Critical Mode) 플라이백 타입의 DC-AC 인버터에 인터리빙을 적용한 디지털 제어를 제안한다. 연속모드(CCM)나 불연속모드(DCM)와 달리 경계 모드의 경우 주파수가 가변되기 때문에 인터리빙으로 구현하기는 상당히 까다로운 측면이 있다. 또한 아날로그 제어기로 구현에 한계를 지니기 때문에 보다 간편한 구현을 위해 디지털 제어IC을 이용하여 구현하는 방법에 대해 기술한다. 본문에서 200W급 플라이백 타입의 DC-AC 인버터에 경계모드 인터리빙을 방법을 적용한 후 실험으로 검증한다.

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CFD estimation of HDCs for varying bodies of revolution of underwater gliders

  • R.V. Shashank Shankar;R. Vijayakumar
    • Ocean Systems Engineering
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    • 제13권3호
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    • pp.269-286
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    • 2023
  • Autonomous Underwater Gliders (AUGs) are a type of Underwater Vehicles that move without the help of a standard propeller. Gliders use buoyancy engines to vary their weight or buoyancy and traverse with the help of the Lift and Drag forces developed from the fuselage and the wings. The Lift and Drag Coefficients, also called Hydrodynamic coefficients (HDCs) play a major role in glider dynamics. This paper examines the effect of the different types of glider fuselages based on the bodies of revolution (BOR) of NACA sections. The HDCs of the glider fuselages are numerically estimated at a low-speed regime (105 Reynolds Number) using Computational Fluid Dynamics (CFD). The methodology is validated using published literature, and the results of CFD are discussed for possible application in the estimation of glider turning motion.

연속전류모드에서 기생손실들을 고려한 고정주파수 LCL형 컨버터 해석 (Analysis of the Fixed Frequency LCL-type Converter at Continuous Current Mode Including Parasitic Losses)

  • 박상은;차한주
    • 전기학회논문지
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    • 제65권5호
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    • pp.785-793
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    • 2016
  • This paper analyzes an LCL-type isolated dc-dc converter operating for constant output voltage in the continuous conduction mode(CCM) with resistances of parasitic losses-static drain-source on resistance of power switch, ESR of resonant network(L-C-L)-using a high loaded quality factor Q assumptions and fourier series techniques. Simple analytical expressions for performance characteristics are derived under steady-state conditions for designing and understanding the behavior of the proposed converter. The voltage-driven rectifier is analyzed, taking into account the diode threshold voltage and the diode forward resistance. Experimental results measured for a proposed converter at low input voltage and various load resistances show agreement to the theoretical performance predicted by the analysis within maximum 4% error. Especially in the case of low output voltages and large loads, It is been observed that introduction of both rectifier and the parasitic components of converter had considerable effect on the performance.

Strainless steel strip 광휘어닐링로 내의 열전달 해석 (A Numerical Analysis of Heat Transfer in Bright Annealing Furnace of Stainless Steel Strip)

  • 유흥선;정연태;장병록
    • 열처리공학회지
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    • 제22권4호
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    • pp.228-233
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    • 2009
  • In order to predict the temperature distribution of stainless steel strip in Bright Annealing (BA) furnace, we performed the analysis of heat transfer and fluid flow using STAR-CCM+. The analysis model included unsteady fluid flow, heat transfer with radiation and moving grid. Two kinds of radiative properties, emissivity and reflectivity, were applied to the stainless steel strip, one is constant and the other is variable with time. As we call, the BA furnaces of stainless steel strip have two different types, muffle and no-muffle. The using of muffle type has been faced with some problems such as rising in material price and shortening of life cycle, etc. So the development of no-muffle type BA furnace is very important in order to save energy cost, lower environmental load and increase the productivity. The designed (or expected) temperature of stainless steel strip coming out of BA furnace was about $1065^{\circ}C$ while the environment temperature maintains around $1100^{\circ}C$. The result of our calculation was very close (or similar) to design temperature, and the application of radiative properties variable with time produced more accurate result than applying constant ones.

반응표면법을 이용한 대형 L-type 자동화용접장치의 구조최적화 연구 (The structure Optimization Research of the Automation Welding Equipment of the Large L-type Using the Response Surface Method)

  • 장준호;정원지;이동선;정장식;정성호
    • 한국생산제조학회지
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    • 제22권1호
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    • pp.138-144
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    • 2013
  • The automation technology for overlay welding is needed due to the occurrence of severe corrosion and abrasion on the surface of internal contact in different shape of fittings. In Korea, different shapes of fittings have been manufactured by using the imported equipment of overlay welding automation at some companies. Thus the research on the development of overlay welding automation system (in short, OWAS) for a large L-type tube is urgently needed. In this paper, the investigation is focused on the optimal design of a supporting base for the (currently developing) OWAS of large L-type tube. Specifically we assume that the base which supports the equipment during the process of overlay welding is loaded as self-weight in the direction of gravity through static analysis especially when it is rotated 180 degree on the OWAS. For optimal design of a supporting base for OWAS of large L-type tube, Solidworks(R) (for 3-dimensional modelling) and ANASYS Workbench(R) (for structural analysis) are incorporated so as to proceed an optimization routines based on Response Surface Method (RSM) and Design of Experiment (DOE). In more specific, DOE finds out major factors (or dimensions) of the supporting base by using MINITAB(R). Then the regression equations between design variables (the major factors of supporting base) and response variables (deformation, stress and safety factor for the supporting base), which will be resulted in by RSM, verify the major factors of DOE. In the next step, Central Composite Design (CCD) plans 20 simulations of ANASYS Workbench(R) and then figures out the optimal values of design variables which will be reflected on the manufacturing of supporting base. Finally welding experiment is conducted to figure out the influence of overlay welding quality in applying the optimized design values of supporting base to the actual OWAS.