• Title/Summary/Keyword: 3-D Steady flow

Search Result 190, Processing Time 0.021 seconds

Three-dimensional Analysis of Flow Characteristics for Intake Valve Design (흡기밸브 형상에 따른 3차원 유동특성 해석)

  • 김득상;이상진;조용석;엄인용
    • Transactions of the Korean Society of Automotive Engineers
    • /
    • v.11 no.4
    • /
    • pp.1-6
    • /
    • 2003
  • Steady flow bench test is a practical, powerful and widely used in most engine manufacturers to give a design concept of a new engine. In order to use steady data as a performance index, it is necessary to build some database, which can correlate the port characteristics with engine data. However, it is very difficult to investigate all port shapes with experimental tools. The steady flow scheme is relatively simple and its results are bulk ones such as flow rate and momentum of flow. Therefore a CFD code can be easily applied to the port evaluation. In this study, the steady flow test was simulated through three-dimensional analysis on intake port design for comparing with experimental data and confirming the feasibility of applying analytic method . for this purpose, the effect of valve curvature on flow rate was estimated by a CFD code. Numerical results were compared with those of real steady flow tests. As a result, the results of 3-D analysis were almost consistent with experimental data.

Intake Flow Characteristics with SCV Open Ratio in a 4-Valve Direct Diesel Engine (4밸브 직분식 디젤엔진의 SCV 개구율에 따른 흡입유동특성)

  • 최승환;전충환;장영준;이진욱
    • Transactions of the Korean Society of Automotive Engineers
    • /
    • v.7 no.7
    • /
    • pp.66-75
    • /
    • 1999
  • Many researchers have developed the measurement technique of in-cylinder flow. Recently, there are lots of studies on steady flow with different SCV geometries. In this study the flow characteristics of four-valve cylinder head were examined in a steady test rig for different SCV open ratios. Each swirl ratio of several SCV angle was quantified by swirl impulse meter and 2D-LDV measurement. The results showed that the swirl ratio was controlled between 2.3 and 3.8 based on SCV angles. The velocity distributions of in-cylinder flow field were measured by 2-D LDV test and visualized swirl and tumble flow pattern at different positions. In this engine , we found out that the swirl was dominant flow.

  • PDF

Numerical analysis of flow characteristics with intake port and valve design (흡기포트 및 밸브 형상에 따른 정상 유동 특성)

  • Lee, Sang-Jin;Kim, Seong-Cheol;Kim, Duk-Sang;Ohm, In-Yong;Cho, Yong-Seok
    • Proceedings of the KSME Conference
    • /
    • 2001.11b
    • /
    • pp.921-927
    • /
    • 2001
  • Steady flow bench test is a practical, powerful and widely used test in most engine manufacturers to give a design concept of a new engine. In order to use steady data as a performance index, it is necessary to build some database, which can correlate the port characteristics with engine data. However, it is very hard to investigate all port and valve shapes with experimental tools. The steady flow scheme is relatively simple and its results are bulk ones such as flow rate and momentum of flow. Therefore a CFD code can be easily applied to the port evaluation. In this study, the steady flow test was simulated through two and three-dimensional analysis on intake port design for comparing with experimental data and confirming the feasibility of applying analytic method. For this purpose, the effect of valve curvature on flow rate was estimated by a CFD code. There results were compared with those of real steady flow tests. As a result, the 2-D analysis described the phenomena qualitatively well, and also the results of 3-D analysis were almost consistent with experimental data.

  • PDF

DEVELOPMENT OF AN UNSTRUCTURED HYBRID MESH FLOW SOLVER FOR 3-D STEADY/UNSTEADY INCOMPRESSIBLE FLOW SIMULATIONS (삼차원 정상/비정상 비압축성 유동해석을 위한 비정렬 혼합격자계 기반의 유동해석 코드 개발)

  • Jung, Mun-Seung;Kwon, Oh-Joon
    • Journal of computational fluids engineering
    • /
    • v.13 no.2
    • /
    • pp.27-41
    • /
    • 2008
  • An unstructured hybrid mesh flow solver has been developed for the simulation of three-dimensional steady and unsteady incompressible flow fields. The incompressible Navier-Stokes equations with an artificial compressibility method were discretized by using a node-based finite-volume method. For the unsteady time-accurate computation, a dual-time stepping method was adopted to satisfy a divergence-free flow field at each physical time step. An implicit time integration method with local time stepping was implemented to accelerate the convergence in the pseudo-time sub-iteration procedure. The one-equation Spalart-Allmaras turbulence model has been adopted to solve high-Reynolds number flow fields. The flow solver was parallelized to minimize the CPU time and to overcome the computational overhead. This method has been applied to calculate steady and unsteady flow fields around submarine configurations and a 3-D infinite cylinder. Validations were made by comparing the predicted results with those of experiments or other numerical results. It was demonstrated that the present method is efficient and robust for the prediction of steady and unsteady incompressible flow fields.

Development of a 3-D Incompressible Flow Solver Based on an Artificial Compressibility Method (가상 압축성 기법을 이용한 삼차원 비압축성 유동해석 코드 개발)

  • Jung, Mun-Seung;Kwon, Oh-Joon
    • 한국전산유체공학회:학술대회논문집
    • /
    • 2008.03b
    • /
    • pp.614-617
    • /
    • 2008
  • An unstructured hybrid mesh flow solver has been developed for the simulations of three dimensional steady and unsteady incompressible flow fields. The incompressible Navier-Stokes equations with an artificial compressibility method were discretized by using a node-based finite-volume method. For the unsteady time-accurate computation, a dual-time stepping method was adopted to satisfy a divergence free flow field at each physical time step. The one equation Spalart-Allmaras turbulence model has been adopted to solve the high-Reynolds number flow fields. This method has been applied to calculate the steady flow fields around submarine configurations and unsteady flow fields around a 3-D infinite cylinder.

  • PDF

Study on Steady Flow Effects in Numerical Computation of Added Resistance of Ship in Waves

  • Lee, Jae-Hoon;Kim, Beom-Soo;Kim, Yonghwan
    • Journal of Advanced Research in Ocean Engineering
    • /
    • v.3 no.4
    • /
    • pp.193-203
    • /
    • 2017
  • This study investigated the steady-flow effects present in the numerical computation of the resistance added to a ship in waves. For a ship advancing in the forward direction, a time-domain 3D Rankine panel method is applied to solve the ship motion problem, and the added resistance due to waves is calculated using a near-field method, with the direct integration of the second-order pressure on the hull surface. In the linear potential theory, the steady flow is approximated by the basis potential of a uniform flow or double-body flow in order to linearize the boundary conditions. By applying these two different linearization schemes, the coupling effects between steady and unsteady solutions were examined. Furthermore, in order to analyze the steady-flow effects on the hull geometry, the computation results for two realistic hull forms, a KVLCC2 tanker and DTC containership, were compared. In particular, the mj term, which represents the coupling effects under the body boundary condition, was evaluated considering the geometry of a non-wall-sided ship. Lastly, the characteristics of the linearization schemes were examined in relation to the disturbed waves around a ship and the components of added resistance.

Development of the 3-D Bulk Motion Index for In-Cylinder Flow Induced by Induction System (I) - Based on the 3-D CFD Simulation Results - (흡기시스템을 통해 실린더로 유도되는 공기의 3차원 Bulk Motion Index 개발 (I) - 3차원 유동해석결과를 중심으로 -)

  • Yun, Jeong-Eui;Nam, Hyeon-Sik;Kim, Myung-Hwan;Min, Sun-Ki;Park, Pyeong-Wan;Kim, Ki-Seong
    • Transactions of the Korean Society of Mechanical Engineers B
    • /
    • v.30 no.11 s.254
    • /
    • pp.1057-1065
    • /
    • 2006
  • In order to figure out the physical meaning of 3-D angular flow index for in-cylinder bulk motion, CFD analysis for the swirl and tumble steady flow test rig were made using commercial package STAR-CD. Computer simulations and rig tests on some kinds of induced flow conditions were carried out. Finally, based on the comparison between the simulated results and measured results, the physical meaning of 3-D angular flow index $|\longrightarrow_{N_B}|$, $\beta$ composed of swirl and tumble coefficients measured by steady flow test rig was described.

Development of the 3-D Bulk Motion Index for In-Cylinder Flow Induced by Induction System (II) - Based on the Steady Flow Rig Test Results - (흡기시스템을 통해 실린더로 유도되는 공기의 3차원 Bulk Motion Index 개발 (II) - 정상유동실험결과를 중심으로 -)

  • Yun, Jeong-Eui;Nam, Hyeon-Sik;Kim, Myung-Hwan;Min, Sun-Ki;Park, Pyeong-Wan;Kim, Ki-Seong
    • Transactions of the Korean Society of Mechanical Engineers B
    • /
    • v.30 no.11 s.254
    • /
    • pp.1066-1073
    • /
    • 2006
  • Recently, because the variable induction systems are adopted to intake system, in-cylinder flow induced by induction system is very complex. Therefore it is very difficult to describe the in-cylinder bulk flow characteristics using the conventional swirl or tumble coefficient. In this study, in order to clarify the 3-D angular flow characteristics of in-cylinder bulk motion in the developing process of variable induction system, we introduced the new 3-D angular flow index, angular flow coefficient($N_B$) Finally, to confirm the index, we carried out the steady flow rig test for intake port of test engine varying valve lift on the test matrix.

Survey on the LIC based flow visualization (LIC 기반의 유동 가시화 기법에 대한 조사 연구)

  • Lee, Joong-Youn
    • Proceedings of the Korea Contents Association Conference
    • /
    • 2007.11a
    • /
    • pp.530-534
    • /
    • 2007
  • Flow visualization is one of visualization techniques and it means a visual expression of vector data using 2D or 3D graphics. It aims for human to easily understand a special feature of the vector data. Flow visualization can be classified into various criterions such as visualization technique, data dimension, type of the flow, and so on. Visualization technique can be categorized into direct method, integration method and derived data based method. Data dimension can be divided into 2D, 2.5D and 3D. Type of flow data may be classified into steady and unsteady. In this paper, various LIC based flow visualization methods will be introduced which is one of representative integration based techniques. Those methods will be categorized with more detailed criterions such as dimension and type of flows.

  • PDF

Laminar Flow Structures Near a Circular Cylinder in between a Free-Surface and a Moving Wall (자유수면과 움직이는 벽면 사이에 놓인 원형 실린더 주위의 층류 유동구조)

  • Seo, Jang-Hoon;Jung, Jae-Hwan;Yoon, Hyun-Sik;Park, Dong-Woo;Chun, Ho-Hwan
    • Journal of the Society of Naval Architects of Korea
    • /
    • v.49 no.3
    • /
    • pp.213-221
    • /
    • 2012
  • The present study numerically investigates the interaction between a free-surface and flow around a circular cylinder over a moving wall. In order to simulate the flow past the circular cylinder over a moving wall near a free-surface, this study has adopted the direct-forcing/fictitious domain (DF/FD) method with the level set method in the Cartesian coordinates. Numerical simulation is performed for a Reynolds numbers of 100 in the range of $0.25{\leq}g/D{\leq}2.00$ and $0.5{\leq}h/D{\leq}2.00$, where g/D and h/D are the gaps between the cylinder and a moving wall and the cylinder and a free-surface normalized by cylinder diameter D, respectively. According to g/D and h/D, the vortex structures have been classified into three patterns of the two-row, one-row, steady elongation. In general, both of g/D and h/D have the large values which mean the cylinder is far away from the wall and the free-surface, two-row vortex structure forms in the wake. When g/D decreases, the two-row vortex structure gradually transfers into the one-row vortex structure. When the g/D reveals the critical value below which the flow becomes steady state, resulting in the steady elongation vortex.