• Title/Summary/Keyword: Flow-3d

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A Numerical Simulation of Flows in an Engine Cooling Passage (엔진 냉각유로 내의 유동에 관한 수치해석)

  • 허남건;윤성영;조원국;김광호
    • Transactions of the Korean Society of Automotive Engineers
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    • v.1 no.1
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    • pp.32-40
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    • 1993
  • Flow fields in model engine cooling passages are studied numerically by using TURBO-3D program, a finite volume based 3-D turbulent flow program adopting a general body fitted coordinate system. The effects of exit position on mass flow rate at each gasket hole are examined for a model cooling passage in order to understand the flow distribution inside the water jacket. The results of the present study can be applied to the design of high performance, high reliability engine.

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Enlarge duct length optimization for suddenly expanded flows

  • Pathan, Khizar A.;Dabeer, Prakash S.;Khan, Sher A.
    • Advances in aircraft and spacecraft science
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    • v.7 no.3
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    • pp.203-214
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    • 2020
  • In many applications like the aircraft or the rockets/missiles, the flow from a nozzle needs to be expanded suddenly in an enlarged duct of larger diameter. The enlarged duct is provided after the nozzle to maximize the thrust created by the flow from the nozzle. When the fluid is suddenly expanded in an enlarged duct, the base pressure is generally lower than the atmospheric pressure, which results in base drag. The objective of this research work is to optimize the length to diameter (L/D) ratio of the enlarged duct using the CFD analysis in the flow field from the supersonic nozzle. The flow from the nozzle drained in an enlarged duct, the thrust, and the base pressure are studied. The Mach numbers for the study were 1.5, 2.0 and 2.5. The nozzle pressure ratios (NPR) of the study were 2, 5 and 8. The L/D ratios of the study were 0.5, 1, 2, 3, 4, 5, 6, 7, 8, 9 and 10. Based on the results, it is concluded that the L/D ratio should be increased to an optimum value to reattach the flow to an enlarged duct and to increase the thrust. The supersonic suddenly expanded flow field is wave dominant, and the results cannot be generalized. The optimized L/D ratios for various combinations of flow and geometrical parameters are given in the conclusion section.

A Study on the Evaluation for the Application of a Comn CFD Code to Flow Analysis of a HAWTs (수평축 풍력발전용 터빈의 유동 해석을 위한 상용 CFD 코드의 적용성 평가에 관한 연구)

  • Kim, B. S.;Kim, J. H.;Nam, C. D.;Lee, Y. H.
    • 유체기계공업학회:학술대회논문집
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    • 2002.12a
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    • pp.396-401
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    • 2002
  • The purpose of this 3-D numerical simulation is evaluate the application of a commercial CFD code to predict 3-D flow characteristics of wind turbine. The experimental approach, which has been main method of investigation, appears to be its limits, the cost increasing disproportionally with the size of the wind turbines, and is hence mostly limited to observing the phenomena. Hence, the use of Computational Fluid Dynamics (CFD) techniques and Wavier-Stokes solvers are considered a very serious contender. The flow solver CFX-TASCflow is employed in all computations presented in this paper. The 3-D flow separation and the wake distribution of 2 bladed Horizontal Axis Wind Turbines (HAWTs) are compared to Heuristic model and visualized result by NREL(National Renewable Energy Laboratory). Simulated 3-D flow separation structure on the rotor blade is very similar to Heuristic model and the wake structure of the wind turbine is good agree with visualized results.

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Analysis of Korean 3D Cinema Work-flow -Focusing on < Sector 7 >- (한국 3D 영화 제작과정 분석-<7광구>의 제작 사례를 중심으로-)

  • Kim, Ik-Sang;Seo, Won-Tae
    • The Journal of the Korea Contents Association
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    • v.12 no.1
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    • pp.166-175
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    • 2012
  • (2010) and have showed possibility of Korean 3D cinema production. From the experience, many problems were deduced in terms of 3D cinema techniques and work-flow. this study is analysis of 's production. The analysis is focused on the problems from the 3D cinema production and pipeline of . By making an analysis the experience, trial and error of production, it will be giving practical information and analysis result to staffs who are willing to create an next Korean 3D cinema. As a result of analysis, has failed to achieve technical accomplishment and to build effective production pipeline. Never the less, it is positively evaluated that it has tried to establish the foundation of Korean 3D cinema production.

A Study on 2D/3D image Conversion Method using Create Depth Map (2D/3D 변환을 위한 깊이정보 생성기법에 관한 연구)

  • Han, Hyeon-Ho;Lee, Gang-Seong;Lee, Sang-Hun
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.12 no.4
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    • pp.1897-1903
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    • 2011
  • This paper discusses a 2D/3D conversion of images using technologies like object extraction and depth-map creation. The general procedure for converting 2D images into a 3D image is extracting objects from 2D image, recognizing the distance of each points, generating the 3D image and correcting the image to generate with less noise. This paper proposes modified new methods creating a depth-map from 2D image and recognizing the distance of objects in it. Depth-map information which determines the distance of objects is the key data creating a 3D image from 2D images. To get more accurate depth-map data, noise filtering is applied to the optical flow. With the proposed method, better depth-map information is calculated and better 3D image is constructed.

A Study on Evaluation for the Applicatioin of a CFD Code to Flow Analysis and an Estimate of Performance for HAWT (수평축 풍력발전용 터빈의 유동해석 및 성능예측에 대한 CFD의 적용성 평가에 관한 연구)

  • Kim, Beom-Seok;Kim, Jeong-Hwan;Kim, You-Taek;Nam, Chung-Do;Lee, Young-Ho
    • Proceedings of the KSME Conference
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    • 2003.04a
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    • pp.2192-2197
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    • 2003
  • The purpose of this 3-D numerical simulation is evaluate the application of a commercial CFD code to predict 3-D flow and power characteristics of wind turbines. The experimental approach, which has been main method of investigation, appears to be its limits, the cost increasing with the size of the wind turbines, hence mostly limited to observing the phenomena on rotor blades. Therefore, the use of Computational Fluid Dynamics (CFD) techniques and Navier-Stokes solvers are considered a very serious contender. The flow solver CFX-TASCflow is employed in all computations in this paper. The 3-D flow separation and the wake distribution of 2 and 3 bladed Horizontal Axis Wind Turbines (HAWTs) are compared to Heuristic model and smoke-visualized experimental result by NREL(National Renewable Energy Laboratory). Simulated 3-D flow separation structure on the rotor blade is very similar to Heuristic model and the wake structure of the wind turbine is good consistent with smoke-visualized result. The calculated power of the 3 bladed rotor by CFD is compared with BEM results by TV-Delft. The CFD results of which is somewhat consist with BEM results, under an error less than 10%.

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A Study on Flow Analysis and an Estimate of performance for HAWT by CFD (CFD에 의한 수평축 풍력발전용 터빈의 유동해석 및 성능예측에 관한 연구)

  • 김정환;김범석;김진구;남청도;이영호
    • Journal of Advanced Marine Engineering and Technology
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    • v.27 no.7
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    • pp.906-913
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    • 2003
  • The purpose of this 3-D numerical simulation is to evaluate the application of a commercial CFD code to predict 3-D flow and power characteristics of wind turbines. The experimental approach, which has been main method of investigation, appears to be its limits, the cost increasing with the size of the wind turbines, hence mostly limited to observing the phenomena on rotor blades. Therefore. the use of Computational Fluid Dynamics (CFD) techniques and Navier-Stokes solvers are considered a very serious contender. The flow solver CFX-TASCflow is employed in all computations in this paper. The 3-D flow separation and the wake distribution of 2 and 3 bladed Horizontal Axis Wind Turbines (HAWTs) are compared to Heuristic model and smoke-visualized experimental result by NREL(National Renewable Energy Laboratory). Simulated 3-D flow separation structure on the rotor blade is very similar to Heuristic model and the wake structure of the wind turbine is good consistent with smoke-visualized result. The calculated power of the 3 bladed rotor by CFD is compared with BEM results by TU-Delft. The CFD results of which is somewhat consist with BEM results. under an error less than 10%.

Flow Stress Determination of Johnson-Cook Model of Ti-6Al-4V Material using 3D Printing Technique (3D 프린팅으로 제작한 Ti-6Al-4V 재료의 Johnson-Cook 모델의 유동 응력 결정)

  • Park, Dae-Gyoun;Kim, Tae-Ho;Jeon, Eon-Chan
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.17 no.4
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    • pp.64-69
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    • 2018
  • This paper investigates the compressive deformation behavior of direct metal tooling (DMT), processing titanium alloy (Ti-6Al-4V) parts under high strain loading conditions. Split Hopkinson Pressure Bar (SHPB) experiments were performed to determine the flow stress and the coefficients of the Johnson-Cook model. This model is described as a function of strain, strain rate, and temperature. SHPB experiments were performed to characterize the deformation behavior of specimens made with 3D printers, using Ti-6Al-4V material under high temperature and dynamic loading.

Hydraulic Characteristic Analysis of Buoyant Flap Typed Storm Surge Barrier using FLOW-3D model (FLOW-3D 모형을 이용한 부유 플랩형 고조방파제의 수리학적 특성 분석)

  • Ko, Dong Hui;Jeong, Shin Taek;Kim, Jeong Dae
    • Journal of Korean Society of Coastal and Ocean Engineers
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    • v.26 no.3
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    • pp.140-148
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    • 2014
  • A storm surge barrier is a specific type of floodgate, designed to prevent a storm surge or spring tide from flooding the protected area behind the barrier. A surge barrier is almost always part of a larger flood protection system consisting of floodwalls, dikes, and other constructions. Surge barriers allow water to pass under normal circumstances but, when a (storm) surge is expected, the barrier can be closed. Among the various means of closing, buoyant flap typed storm surge barrier which was indicated by MOSE project in Italy is chosen for Masan bay protection, and the motion of the surge barrier under the action of storm surge and wave is examined using FLOW-3D, a computational fluid dynamics software analyzing various physical flow processes. Numerical result shows that storm surge barrier is successfully operated under wave height 3 m, and tidal range 2 m.