• 제목/요약/키워드: flow effect

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Verification of Speed-up Mechanism of Pedestrian-level Winds Around Square Buildings by CFD

  • Hideyuki Tanaka;Qiang Lin;Yasuhiko Azegami;Yukio Tamura
    • International Journal of High-Rise Buildings
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    • v.11 no.4
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    • pp.301-314
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    • 2022
  • Various studies have been conducted on pedestrian-level wind environments around buildings. With regard to the speed-up mechanism of pedestrian-level winds, there are references to downwash effect due to the vertical pressure gradient of boundary layer flow and venturi effect due to flow blocking by the building. Two factors contribute to increase or decrease of downwash effect: change in twodimensional / three-dimensional air flow pattern (Type 1) and change in downwash wind speed due to building size that does not accompany change in airflow pattern (Type 2). Previous studies have shown that downwash effect has a greater influence in increasing or decreasing the area of strong wind than venturi effect. However, these considerations are derived from the horizontal mean wind speed distribution at pedestrian level and are not the result of three-dimensional flow field around the building. Therefore, in this study, Computational Fluid Dynamics using Large Eddy Simulation were performed to verify the downwash phenomena that contributes to increase in wind speed at pedestrian level.

Scale Effect on the Flow-Induced Vibration of Carbon Nanotubes Conveying Fluids (Scale effect를 고려한 탄소나노튜브의 유체유발진동)

  • Choi, Jong-Woon;Kim, Sung-Kyun;Park, Sang-Yun;Kim, Young-June;Song, Oh-Seop
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2011.10a
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    • pp.147-152
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    • 2011
  • In this paper, static and oscillatory loss of stability of carbon nanotube conveying fluid and modelled as a thin-walled beam is investigated. Analytically nonlocal effect, transverse shear and rotary inertia are incorporated in this study. The governing equations and the boundary conditions are derived through Hamilton's principle. Numerical analysis is performed by using extend Galerkin method which enables us to obtain more exact solutions compared with conventional Galerkin method. Variations of critical flow velocity for analytically nonlocal effect, partially nonlocal effect and local effect of carbon nanopipes are investigated and pertinent conclusion is outlined.

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Effect of Venturi System on Acceleration of Low-speed Water Flow at the Venturi Throat Installed at the Inlet of Hydro Turbine

  • Jung, Sang-Hoon;Seo, In-Ho;Kim, Chul-Ho
    • Journal of Advanced Marine Engineering and Technology
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    • v.35 no.7
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    • pp.914-920
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    • 2011
  • For a hydro turbine electricity generation system in river or bay, a venturi system could be applied to accelerate flow speed at the inlet of the turbine system in a flow field. In this study, a steady flow simulation was conducted to understand the effect of venturi system on the acceleration of current speed at the inlet of a hydro turbine system. According to the continuity equation, the flow speed is inversely proportional to the cross-section area in a conduit flow; however, it would be different in an open region because the venturi system would be an obstruction in the flow region. As the throat area is 1/5 of the inlet area of the venturi, the flow velocity is accelerated up to 2.1 times of the inlet velocity. It is understood that the venturi system placed in an open flow region gives resistance to the upcoming flow and disperses the flow energy around the venturi system. The result of the study should be very important information for an optimum design of a hydro turbine electricity generation system.

Structure of Tip Leakage Flow in a Forward-Swept Axial-Flow Fan (전향 스윕 축류형 팬에서의 팁 누설 유동 구조)

  • Lee, Gong-Hee;Baek, Je-Hyun
    • 유체기계공업학회:학술대회논문집
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    • 2002.12a
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    • pp.131-136
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    • 2002
  • A computational analysis using Reynolds stress model in FLUENT is conducted to give a clear understanding of the effect of blade loading on the structure of tip leakage flow in a forward-swept axial-flow fan at design condition ($\phi$=0.25) and off-design condition ($\phi$=0.21 and 0.30). The roll-up of tip leakage flow starts near the minimum static wall pressure position, and the tip leakage vortex developes along the centerline of the pressure trough within the blade passages. Near tip region, a reverse flow induced by tip leakage vortex has a blockage effect on the through-flow. As a result, high momentum region is observed below the tip leakage vortex. As the blade loading increases, the reverse flow region is more inclined toward circumferential direction and the onset position of the rolling-up of tip leakage flow moves upstream. Because the casing boundary layer becomes thicker, and the mixing between the through-flow and the leakage jet with the different flow direction is enforced, the streamwise vorticity decays more fast with blade loading increasing. The computational results show that a distinct tip leakage vortex is observed downstream of the blade trailing edge at $\phi$=0.30, but it is not observed at $\phi$=0.21 and 0.25.

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DSMC Calculation of the Hypersonic Free Stream and the Side Jet Flow Using Unstructured Meshes (비정렬 격자 직접모사법을 이용한 희박 유동과 측면 제트의 상호 작용에 관한 연구)

  • Kim M. G.;Kwon O. J.;Ahn C. S.
    • 한국전산유체공학회:학술대회논문집
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    • 2004.03a
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    • pp.126-131
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    • 2004
  • The interaction between the hypersonic free stream and the side jet flow at high altitudes is investigated by direct simulation Monte Carlo(DSMC) method. Since there is a great difference in density between the free stream and the side jet flow, the weighting factor technique which could control the number of simulation particles, is applied to calculate these two flows simultaneously. Chemical reactions are not considered in the calculation. For validation, the corner flow passing between a pair of plates that are perpendicularly attached is solved. The side jet flow is then injected into this comer flow and solution is found for the merged flow. Results are compared with the experiments. For a more realistic rocket model, the flow past a blunted cone cylinder shape is solved. The leeward or windward jet injection is merged with this flow. The effect on the rocket surface is observed at various flow angles. The lambda effect and the wake structure are found like low attitudes. High interaction between the free stream and the side jet flow is observed when the side jet is injected in the windward direction.

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Helium-Air Exchange Flow with Fluids Interaction (유체간섭을 동반하는 헬륨과 공기의 치환류)

  • T.I. Kang
    • Journal of Advanced Marine Engineering and Technology
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    • v.21 no.4
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    • pp.372-380
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    • 1997
  • This paper describes experimental investigations of helium-air exchange flows through parti¬tioned opening and two-opening. Such exchange flows may occur following rupture accident of stand pipe in high temperature gas cooled reactor. A test vessel with the two types of small open¬ing on top of test cylinder is used for experiments. An estimation method of mass increment is developed and applied to measure the exchange flow rate. A technique of flow visualization by Mach-Zehnder interferometer is provided to recognize the exchange flows. In the case of exchange flow through the partitioned opening, flow passages of upward flow of the helium and downward flow of the air within the opening are separated by vertical partition, and the two flows interact out of entrance and exit of the opening. Therefore, an experiment of the exchange flow through two-opening is made to investigate effect of the fluids interaction of the partitioned opening sys¬tem. As a result of comparison of the exchange flow rates between the two types of the opening system, it is found that the exchange flow rate of the two-opening system is larger than that of the partitioned opening system due to absence of the effect of fluids interaction. Finally, the fluids interaction between the upward and downward flows through the partitioned opening is found to be an important factor on the helium-air exchange flow.

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Effect of Vanes on Flow Distribution in a Diffuser Type Recuperator Header (디퓨저 타입 레큐퍼레이터 헤더에서 유동분배에 미치는 베인의 영향)

  • Jeong Young-Jun;Kim Seo-Young;Kim Kwang-Ho;Kwak Jae-Su;Kang Byung-Ha
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.18 no.10
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    • pp.819-825
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    • 2006
  • In a SOFC/GT (solid oxide fuel cell/gas turbine) hybrid power generation system, the recuperator is an indispensible component to enhance system performance. Since the expansion ratio to the recuperator core is very large, generally, the effective header design to distribute the flow uniformly before entering the core is crucial to guarantee the required performance. In the present study, we focus on the design of a diffuser type recuperator header with a 90 degree turn inlet port. To reduce the flow separation and recirculation flows, multiple horizontal vanes are used. The number of horizontal vanes is varied from 0 to 24. The air flow velocity is measured at 40 points just behind the core outlet by using a hot wire anemometer. Then, the flow non-uniformity is evaluated from the measured flow velocity. The experimental results showed that inlet air velocity did not effect on relative flow non-uniformity. According to increasing the number of horizontal vanes, flow non-uniformity reduced about $40{\sim}50%$ than without using horizontal vanes.

The Influence of Family Strength on College Students' Flow (가족건강성이 대학생의 몰입에 미치는 영향)

  • Lee, Hyo Jin;Jung, Sohee;Choi, Woong Yong
    • The Journal of Korean Society for School & Community Health Education
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    • v.18 no.1
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    • pp.81-97
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    • 2017
  • Objecives: This study was performed to analyze the effect of the family strength perceived by college students on flow. Methods: To achieve this purpose, a survey on the family strength and flow was conducted on 113 male college students and 187 female college students. Correlation analysis and independent sample t-test were carried out among the variables, and regression analysis was performed to examine the effect of the family strength on flow. Results: The results are as follows. Firstly, the family strength of the college students had a static correlation with flow. Secondly, the examination on the difference between the male and female college students in the family strength and the flow revealed that the family strength and flow of male students were significantly higher than those of the female students. Thirdly, according to the analysis on the influence of family strength on flow when the sociodemographic background was controlled, the shared value system among family members, the ability of problem solving, and ties with family members from the sub-factors of family strength had significant effect on the sub-factors of flow. Conclusions: Through the above results, this study identified that family strength is important for college students who have greater independence and freedom than in middle and high school, and the higher family strength was, the higher flow was. This result can be used as a basis to prepare a practical intervention plan to increase the flow of college students.

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The Effect of Presence and Flow of Augmented Reality Advertising on the Advertising toward Attitude and Recall (증강현실 광고의 프레즌스(Presence)와 플로우(Flow)가 광고 태도와 회상에 미치는 영향)

  • Han, Kwang-Seok;Choi, Junehyock
    • Journal of Digital Convergence
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    • v.18 no.8
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    • pp.29-35
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    • 2020
  • This study identified the impact of augmented reality advertising on attitude toward advertising and memory according to the type of presence and flow level. The presence (cognitive, emotional, media) and flow level (high vs. low) of the augmented reality(AR) advertising were set as independent variables and analyzed by Two-Way MANOVA. As a result of the research, first, the augmented reality advertising attitude was positive when the emotional presence and flow level were high. Second, when the flow level is high, the ARM such as product attribute information increases, but when the flow level is low, the evaluation-oriented GRM increases. Third, emotional presence increases GRM when the flow level is high, but ARM increases when the flow level is low. Fourth, the memory effect was low regardless of the flow level. In the future research, it would be desirable to produce augmented reality advertisements through virtual brands in the generalization of research.

Numerical simulation of jet flow impinging on a shielded Hartmann whistle

  • Michael, Edin;Narayanan, S.;Jaleel. H, Abdul
    • International Journal of Aeronautical and Space Sciences
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    • v.16 no.2
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    • pp.123-136
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    • 2015
  • The present study numerically investigates the effect of shield on the flow characteristics of Hartmann whistle. The flow characteristics of un-shielded Hartmann whistle are compared with whistles of different shield heights 15 mm, 17 mm, 20 mm, 25 mm and 30 mm. The comparison of Mach number contours and transient velocity vectors of shielded Hartmann whistles with un-shielded ones for the same conditions reveal that the presence of shield causes the exiting jet to stick to the wall of the shield without causing spill-over around the cavity inlet, thus sustaining the shock oscillation as seen in the unshielded Hartmann whistle, which has intense flow/shock oscillation and spill-over around the cavity mouth. The velocity vectors indicate jet regurgitance in shielded whistles showing inflow and outflow phases like un-shielded ones with different regurgitant phases. The sinusoidal variation of mass flow rate at the cavity inlet in un-shielded Hartmann whistle indicates jet regurgitance as the primary operating mode with large flow diversion around the cavity mouth whereas the non-sinusoidal behavior in shielded ones represent that the jet regurgitance is not the dominant operating mode. Thus, this paper sufficiently demonstrates the effect of shield in modifying the flow/shock oscillations in the vicinity of the cavity mouth.