• Title/Summary/Keyword: 유동깊이

Search Result 151, Processing Time 0.023 seconds

저 레이놀즈 수에서 선인장 단면 모양 실린더의 항력 특성 연구

  • An, Chan-Geun
    • Proceeding of EDISON Challenge
    • /
    • 2016.03a
    • /
    • pp.530-536
    • /
    • 2016
  • 본 연구에서는 EDISON_CFD의 2D_YUIBM_1 해석자를 사용하여 선인장 단면 모양 실린더의 $C_D$를 가시의 개수(N)와 가시의 깊이(D)에 따른 경향성으로 나타내었다. 저 레이놀즈 수에 대한 유동 해석을 해야 하므로 레이놀즈 수 영역은 20(steady), 40(steady), 100(Unsteady)을 사용하였다. 또한, 특징적인 효과를 보이는 몇 개의 케이스를 선별해 그 모델들에서 $C_P$와 Vorticity의 분포를 조사했으며 이를 통해 저 레이놀즈 수의 선인장 모양 실린더에서 $C_D$의 변화 원인을 규명하였다. 마지막으로, 물체의 기하학적 성질과 유체의 성질을 기반으로 저 레이놀즈 수에서 $C_D$를 최적화하는 공식을 산출하였다.

  • PDF

Structural Change of Supersonic Jet Due to Liquid Injection in Supersonic Backward Facing Step Flow (초음속 후향 계단 유동에서 액체 분사로 인한 초음속 제트의 구조 변화)

  • Ahn, Sang-Hoon;Han, Doo-Hee;Choi, Han-Young;Seo, Seong-Hyeon;Sung, Hong-Gye
    • Journal of Aerospace System Engineering
    • /
    • v.13 no.6
    • /
    • pp.9-16
    • /
    • 2019
  • The experiment on the liquid jet in crossflow in supersonic BFS (backward-facing step) flow was conducted to investigate the mixing characteristics. The working fluids are nitrogen and water. The shadow graph technique was used to visualize the flow field. Images captured by the high-speed camera were applied to analyze the flow phenomena. The liquid jet was injected at the re-circulation zone created by the supersonic jet flow. Experimental conditions are defined based on the pressure of the nitrogen gas chamber and pressurized liquid tank. In respective cases, the penetration depth of liquid jet and location of the Mach disc were observed to be proportional to the momentum ratio of gas and liquid jets.

Study of Internal Flow in the supersonic Nozzle by the Hydraulic Analogy (수력학적 상사를 적용한 초음속 노즐 내부 유동 연구)

  • Lee, Ji-Hyung;Lee, Kyung-Hun
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2009.11a
    • /
    • pp.477-482
    • /
    • 2009
  • Though rocket nozzle flow is very important to the rocket performance, the direct measurement is very difficult because of high temperature and high pressure gas flow. Then the experiment utilizing the hydraulic analogy has been developed for such a problem. Supersonic flows through an axisymmetric De Laval nozzle of solid rocket motor was simulated in a 2-D sluice-type water-table designed and manufactured utilizing hydraulic analogy. Methods to minimize or account for non-analogous effects in the hydraulic system must be reviewed for the quantitative application of the hydraulic analogy. In this application the water table is inclined slightly, so that gravity acceleration has a small component in the direction of motion, thus compensating for the effect of friction. Flow visualization leads to better understanding of the analogous system. Within the experimental errors, it is shown that the hydraulic analogy can be used as an effective tool for the study of two dimensional isentropic flows of gases in many fields.

  • PDF

A Numerical Calculation of Viscous Flow around a Hydrofoil Advancing beneath the Free Surface (자유수면 아래서 전진하는 수중익 주위의 점성유동 해석)

  • J.J. Park;S.M. Jeong;Y.G. Lee;S.H. Lee;S.W. Hong
    • Journal of the Society of Naval Architects of Korea
    • /
    • v.32 no.3
    • /
    • pp.72-82
    • /
    • 1995
  • In the present paper, flow characteristics and free surface waves generated by a submerged hydrofoil advancing with an uniform speed are calculated. Using a numerical method based on a MAC(Marker And Cell) method, the Navier-Stokes and the continuity equations are solved to simulate flow fields around the hydrofoil. Computations are carried out in a rectangular grid system in which grids are concentrated near the foil and the free surface to improve numerical accuracies. Viscous flow phenomenas including pressure distributions are computed. Moreover, the influences of submerged depths upon the generated wave profiles and the wave breaking phenomena are also investigated. Experiments are performed at the towing tank of Inha University to measure free surface wave elevations due to the advancing hydrofoil. The computational results are compared with the present and the other available experimental data to show the accuracy of the numerical method developed.

  • PDF

Controlling the Horseshoe Vortex by Leading-Edge Chamfer at a Generic Wing-Body Junction (단순 날개-몸체 접합부에서의 앞전 모서리 홈에 의한 말굽와류 제어)

  • Cho, Jong-Jae;Kim, Kui-Soon
    • Journal of the Korean Society of Propulsion Engineers
    • /
    • v.13 no.2
    • /
    • pp.26-34
    • /
    • 2009
  • Secondary flow losses can be as high as 30~50% of the total aerodynamic losses for a turbo-machinery blade or stator row. These are important part for improving a turbine efficiency. Therefore, many studies have been performed to decrease the secondary flow losses. The present study deals with the chamfered leading-edge at a generic wing-body junction to decrease the horseshoe vortex, one of factors to generate the secondary flow losses, and investigates the vortex generation and the characteristics of the horseshoe vortex with the chamfered height, and depth of the chamfer by using $FLUENT^{TM}$. It was found that the total pressure loss for the best case can be decreased about 1.55% compare to the baseline case.

Heat transfer characteristic and flow pattern investigation in micro-channels during two-phase flow boiling (이상 유동 비등 시 마이크로 채널에서의 열전달 특성과 유동양식 조사)

  • Choi, Yong-Seok;Lim, Tae-Woo
    • Journal of Advanced Marine Engineering and Technology
    • /
    • v.39 no.7
    • /
    • pp.696-701
    • /
    • 2015
  • Two-phase flow boiling experiments were conducted in 15 micro-channels with a depth of 0.2 mm, width of 0.45 mm, and length of 60 mm. FC-72 was used as the working fluid, and the mass fluxes ranged from 200 to $400kg/m^2s$. Tests were performed over a heat flux range of $5-40kW/m^2$ and vapor quality range of 0.1-0.9. The heat transfer coefficient sharply decreased at a lower heat flux and then was kept approximately constant as the heat flux is increased. Based on the measured heat transfer data, the flow pattern was simply classified into bubbly, slug, churn, and wavy/annular flows using the existing method. In addition, these classified results were compared to the transition criterion to wavy/annular regime. However, it was found that the existing transition criterion did not satisfactorily predict the transition criterion to annular regime for the present data.

Study of Drag Force of Subsea Pipeline in Trench (트랜치내의 해저 관로 항력 변화 고찰)

  • 조철희;김경수;홍성근
    • Proceedings of the Korea Committee for Ocean Resources and Engineering Conference
    • /
    • 2000.04a
    • /
    • pp.13-17
    • /
    • 2000
  • 해저관로가 노출되어 있을 경우 파도와 조류 등에 의한 외적 하중으로부터 안정적이어야 한다. 트랜치 구간 내의 해저관로에 작용하는 유체 입자의 속도와 가속도는 해저면과 비교하여 볼 때 현저히 감소하므로 감쇄 계수를 사용하여 트랜치 구간 내에 설치되는 해저관로의 안정성을 해석한다. 그러나, 다양한 트랜치 구간의 깊이와 기울기에 대한 감쇄 계수에 대해 많은 자료가 부족하여 실제 설계에는 한정된 계수들이 이용된다. 본 논문에서는 다양한 깊이와 기울기를 가진 트랜치 구간의 실험 모형을 제작하여 회류 수조에서 P.I.V(입자 영상 속도계) 기법을 이용하여 여러 속도에 대하여 실험을 수행하였다. 다양한 트랜치 구간 내의 실린더 주변의 유동 특성과 유체 입자의 수평 속도를 측정하여 항력 감쇄 계수를 산출해 냈으며 실제 해양 공사에서 적용 가능한 안정성 해석 기준을 제시하였다.

  • PDF

Approximate Model of Viscous and Squeeze-film Damping Ratios of Heat Exchanger Tubes Subjected to Two-Phase Cross-Flow (2 상 유동장에 놓인 열 교환기 튜브에 작용하는 점성과 압착막 감쇠비의 어림적 해석 모델)

  • Sim, Woo Gun
    • Transactions of the Korean Society of Mechanical Engineers B
    • /
    • v.39 no.1
    • /
    • pp.97-107
    • /
    • 2015
  • An analytical model was developed to estimate the viscous and squeeze-film damping ratios of heat exchanger tubes subjected to a two-phase cross-flow. Damping information is required to analyze the flow-induced vibration problem for heat exchange tubes. In heat exchange tubes, the most important energy dissipation mechanisms are related to the dynamic interaction between structures such as the tube and support and the liquid. The present model was formulated considering the added mass coefficient, based on an approximate model by Sim (1997). An approximate analytical method was developed to estimate the hydrodynamic forces acting on an oscillating inner cylinder with a concentric annulus. The forces, including the damping force, were calculated using two models developed for relatively high and low oscillatory Reynolds numbers, respectively. The equivalent diameters for the tube bundles and tube support, and the penetration depth, are important parameters to calculate the viscous damping force acting on tube bundles and the squeeze-film damping forces on the tube support, respectively. To calculate the void fraction of a two-phase flow, a homogeneous model was used. To verify the present model, the analytical results were compared to the results given by existing theories. It was found that the present model was applicable to estimate the viscous damping ratio and squeeze-film damping ratio.

Research on ANN based on Simulated Annealing in Parameter Optimization of Micro-scaled Flow Channels Electrochemical Machining (미세 유동채널의 전기화학적 가공 파라미터 최적화를 위한 어닐링 시뮬레이션에 근거한 인공 뉴럴 네트워크에 관한 연구)

  • Byung-Won Min
    • Journal of Internet of Things and Convergence
    • /
    • v.9 no.3
    • /
    • pp.93-98
    • /
    • 2023
  • In this paper, an artificial neural network based on simulated annealing was constructed. The mapping relationship between the parameters of micro-scaled flow channels electrochemical machining and the channel shape was established by training the samples. The depth and width of micro-scaled flow channels electrochemical machining on stainless steel surface were predicted, and the flow channels experiment was carried out with pulse power supply in NaNO3 solution to verify the established network model. The results show that the depth and width of the channel predicted by the simulated annealing artificial neural network with "4-7-2" structure are very close to the experimental values, and the error is less than 5.3%. The predicted and experimental data show that the etching degree in the process of channels electrochemical machining is closely related to voltage and current density. When the voltage is less than 5V, a "small island" is formed in the channel; When the voltage is greater than 40V, the lateral etching of the channel is relatively large, and the "dam" between the channels disappears. When the voltage is 25V, the machining morphology of the channel is the best.

A Study on the Turbulent Flow Characteristics in the Wake of Transom Sterns using PIV Method (동일입자추적기법을 이용한 트랜섬선미 후류 난류유동특성에 관한 연구)

  • Lee, Gyoung-Woo;Gim, Ok-Sok
    • Journal of the Korean Society of Marine Environment & Safety
    • /
    • v.18 no.4
    • /
    • pp.352-359
    • /
    • 2012
  • An experiment was carried out to figure out the turbulence flow characteristics in the wake of the transom stern's 2-dimensional section by 2-frame grey level cross correlation PIV method at Re= $3.5{\times}10^3$, Re= $7.0{\times}10^3$. The angles of transom stern are $45^{\circ}$(Model "A"), $90^{\circ}$(Model "B") and $135^{\circ}$(Model "C") respectively. The depth of wetted surface is 40mm from free surface. Strong turbulence intensity appears at the interaction between the flow separation of the bottom of a model and the free surface. This study provides statistic flow information such as turbulence intensity, Reynolds stress and turbulence kinetic energy. Model C type (Raked transom) has low Reynolds stress and turbulence kinetic energy.