• 제목/요약/키워드: Flow Frequency

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주기적으로 회전진동하는 원주 후류의 공진특성 (Lock-on Characteristics of wake behind a Rotationally Oscillating Circular Cylinder)

  • 이정엽;이상준
    • 한국가시화정보학회:학술대회논문집
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    • 한국가시화정보학회 2004년도 추계학술대회 논문집
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    • pp.18-21
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    • 2004
  • Lock-on characteristics of the flow around a circular cylinder performing a rotationally oscillation with a relatively high forcing frequency have been investigated experimentally using flow visualization and hot-wire measurements. Dominant parameters are Reynolds number (Re), amplitude of oscillation $(\theta_A)$, and frequency ratio $F_R=f_f\;/\;f_n$, where $f_f$ is the forcing frequency and if is the natural frequency of vortex shedding. Experiments were carried out under the conditions of $Re=4.14\times10^3,\;\pi/15\leq\theta_A\leq\pi/3$, and $F_R=1.0$. The effects of this active control technique on the lock-on flow regime of the cylinder wake were evaluated through wake velocity measurements and spectral analysis of hot-wire signals. The rotary oscillation modified the flow structure of near wake significantly. The lock-on phenomenon was found to occur in the range of frequency encompassing the natural vortex shedding frequency. In addition, when the amplitude of oscillation is less than a certain value, the lock-on phenomenon was occurred only at $F_R=1.0$. The lock-on range expanded and vortex formation length decreased as the amplitude of oscillation increases. The rotary oscillation generated small-scale vortex structure just near the cylinder surface.

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음향교란을 받는 난류박리기포의 이산와류 수치해석 (Discrete-vortex Simulation of Turbulent Separation Bubble Excited by Acoustic Perturbatioons)

  • 임재욱;성형진
    • 대한기계학회논문집
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    • 제16권4호
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    • pp.775-786
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    • 1992
  • 본 연구에서는 DVM의 이론적 배경과 수치계산에 대해 자세히 다루었다. 음향 교란이 가졌을 때의 재부착에 대한 수치해석결과는 Kiya등의 실험결과와 비교하 였으며 만족할만한 일치를 보여주었다. 결과 및 고찰에서는 주로 음향교란이 있는 경우의 재부착길이를 최소화하는 주파수와 교란이 없는 유동의 난류구조해석을 평균속 도 및 압력과 그의 섭동치, 그리고 파워 스펙트럼과 상관계수등을 통해 자세히 비교검 토하였다.

뭉툭한 물체 주위 유동에서 항력 감소를 위한 능동 제어 방법 (Active Control Methods for Drag Reduction in Flow over Bluff Bodies)

  • 최해천
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2002년도 학술대회지
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    • pp.11-16
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    • 2002
  • In this paper, we present two successful results from active controls of flows over a circular cylinder and a sphere for drag reduction. The Reynolds number range considered for the flow over a circular cylinder is 40-3900 based on the free-stream velocity and cylinder diameter, whereas for the flow over a sphere it is $10^{5}$ based on the free-stream velocity and sphere diameter. The successful active control methods are a distributed (spatially periodic) forcing and a high-frequency (time periodic) forcing. With these control methods, the mean drag and lift fluctuations decrease and vortical structures are significantly modified. For example, the time-periodic forcing at a high frequency (larger than 20 times the vortex shedding frequency) produces $50{\%}$ drag reduction for the flow over a sphere at $Re=10^{5}$. The distributed forcing applied to the flow over a circular cylinder results in a significant drag reduction at all the Reynolds numbers investigated.

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에어콘 실외기용 축류송풍기의 비정상 유동장 특성 연구 (Unsteady Flow Characteristics of an Axial Flow Fan Installed in the Outdoor Unit of Air Conditioner)

  • 장춘만
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2005년도 연구개발 발표회 논문집
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    • pp.223-230
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    • 2005
  • The unsteady nature of vortex structures has been investigated by a large eddy simulation (LES) in an axial flow fan with a shroud covering only the rear region of its rotor tip. The simulation shows that the tip vortex plays a major role in the structure and unsteady behavior of the vortical flow in the fan. The movements of the vortex structures induce high-pressure fluctuations on the rotor blade and in the blade passage. Frequency characteristics of the fluctuating pressure on the rotor blade are analyzed using wavelet transform. The dominant frequency of the real-time pressure selected at the high pressure fluctuation region corresponds well to that of the fluctuating rotor torque and the experimental result of fan noise. It is mainly generated due to the unsteady behavior of the vortical flow, such as the tip vortex and the leading edge separation vortex.

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칼만와류식 공기유량센서의 와안정판이 후류유동장과 와유출주파수에 미치는 영향 (The Effect on Wake Flow and Vortex Shedding Frequency by Vortex Stabilizer in Karman Vortex Type Air Flow Sensor)

  • 임성원;류병남;이종춘;부정숙
    • Journal of Advanced Marine Engineering and Technology
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    • 제25권4호
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    • pp.846-856
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    • 2001
  • An experimental study has been made to investigate the effect on wake flow and vortex shedding frequency by vortex stabilizer in Karman vortex type air flow sensor. The conditions investigated include 3 types of shapes and 3 types of separation distances of the vortex stabilizer. The phase averaged technique and smoke-wire flow visualization method are used to understand the detail information. The rolling up position of shear layer is fixed by the influence of the vortex stabilizer. Especially, the convex type vortex stabilizer has shown the more stable repeatability and linearity regarding the vortex shedding frequency compared to the other types.

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마이크로 유로에서 맥동유동에 의한 혼합촉진에 관한 수치해석 (A Numerical Simulation on Mixing Enhancement by Inlet Flow Pulsation in a Micro Conduit)

  • 김서영;리광훈
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2003년도 유체기계 연구개발 발표회 논문집
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    • pp.231-237
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    • 2003
  • A numerical study has been conducted to investigate the effect of an inlet flow pulsation on mixing of two solutions with different concentrations in a micro conduit. We treat an unsteady, incompressible and two-dimensional flow through a micro conduit by adopting the momentum equations with the electrostatic force due to streaming current and the concentration equation. The feasibility of the inlet flow pulsation to enhance the mixing process inside the micro conduit is carefully examined by varying the inlet pulsation frequency. When a low-frequency pulsation is induced at the inlet, the interface between two solutions with different concentrations becomes wavy, which results in mixing enhancement. As the pulsation frequency increases, the waviness of the interface becomes meager, and the concentration gradients at the interface approach the value for the non-pulsating steady flow.

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PIV 측정 흐름형태에 의한 타원형 날개꼴의 동적 실속 특성 연구 (A Study on the Dynamic Stall Characteristics of an Elliptical Airfoil by Flow Pattern Measured by PIV)

  • 이기영;손명환;정형석
    • 한국군사과학기술학회지
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    • 제8권3호
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    • pp.116-123
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    • 2005
  • An experimental investigation on the static and dynamic stall characteristics of elliptic airfoil was performed by PIV velocity field measurements. The flow Reynolds number was $3.13{\times}10^5$ and the reduced frequency of the pitch oscillation ranged from 0.075 to 0.125. The onset of static stall was caused by boundary layer separation which started at the trailing edge and progressed toward the leading edge. However, dynamic stall was caused by the vortex shed at the leading edge region and the flow field showed a vortex dominated flow with turbulent separation and alternate vortex shedding. The increase of reduced frequency increased the dynamic stall angle of attack and intensified the flow hysteresis in the down-stroke phase.

자동차 도어 진동의 파워흐름해석에 대한 실험적 연구 (Experimental Study on Power Flow Analysis of Vibration of an Automobile Door)

  • 길현권;이용현;이규형;황성국;홍석윤;박영호;서진관;채기상;서성훈
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2006년도 춘계학술대회논문집
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    • pp.782-785
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    • 2006
  • The Power Flow Analysis(PFA) can be effectively used to predict structural vibration in medium-to-high frequency range. In this paper, Power Flow Finite Element Method (PFFEM) based on PFA has been used to predict the vibration of an automobile door. The predicted results for the frequency response function of the door have been compared with corresponding experimental results. In the experiment, the automobile door has been divided into several subsystems and the loss factor of each subsystem has been measured. The input mobility at a source point has been also measured. The data for the loss factors and the input mobility have been used as the input data to predict the vibration of the automobile door with PFFEM. The frequency response functions have been measured over the surface of the door. The comparison between the experimental results and the predicted results for the frequency response functions showed that PFFEM could be an effective tool to predict the structural vibration.

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에어포일 이산소음 특성에 관한 연구 (A Study on Discrete Frequency Noise from a Symmetrical Airfoil in a Uniform Flow)

  • Kim, H. J.;Lee, S.;N. Fujisawa
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2002년도 추계학술대회논문초록집
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    • pp.365.2-365
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    • 2002
  • The flow field around a symmetrical airfoil in a uniform flow under the generation of noise was studied by experiments and numerical simulation. The experiments are conducted by visualizing the surface flow over the airfoil with a shear-sensitive liquid-crystal coating and by measuring the instantaneous velocity field around the trailing edge of the airfoil. The numerical simulation was carried out by LES. (omitted)

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고빈도 진동 환기가 동맥혈의 호흡성 가스에 미치는 영향 (Factors influencing arterial $CO_2$ tension in cats during high frequency oscillation ventilation)

  • 도준영;이재익;이관호;김영조;정재천;이현우;이석강
    • Journal of Yeungnam Medical Science
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    • 제6권2호
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    • pp.47-55
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    • 1989
  • 고빈도 진동환기가 동맥혈의 가스분압에 미치는 영향을 알아보고자 저자들은 9마리의 고양이를 대상으로 진동빈도, 일회분출량 및 bias flow를 다양하게 변화시켜 아래와 같은 결과를 얻었다. 1) 일회분출량과 bias flow를 고정시킨 후 진동빈도를 점차 증가시켜 도 $PaCO_2$의 변동은 없었다(Table 1). 2) 진동빈도를 고정시킨 후 일회분출량과 bias flow를 변화시켜 관찰하였던 바 $PaCO_2$는 bias flow의 변화와는 상관관계가 없으나, 일회분출량의 변화와는 유의한 상관관계가 있었다(p<0.01)(Table 2, Fig. 1). 3) $PaCO_2$는 진동빈도를 15Hz로 고정시킨 상태하에서는 1회 분출량 및 bias flow를 증가시켜도 큰 변동없이 정상으로 유지되었다(Table 2). 이상의 결과로 고빈도 진동환기법에서 $PaCO_2$의 결정인자는 진동빈도와 bias flow와는 무관하였고 일회분출량과는 상관관계가 있음을 알 수 있었다.

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