• 제목/요약/키워드: air duct

Search Result 538, Processing Time 0.024 seconds

Numerical Prediction of Chamber Performance for OWC Wave Energy Converter (OWC 파력발전장치의 공기실 성능예측에 대한 수치적인 연구)

  • Jin, Ji-Yuan;Hyun, Beom-Soo;Liu, Zhen;Hong, Key-Yong
    • Journal of the Korean Society for Marine Environment & Energy
    • /
    • v.13 no.2
    • /
    • pp.91-98
    • /
    • 2010
  • The water elevation inside the air chamber and bi-directional air flow in the duct of Oscillating Water Column wave energy converter is one of the most important factors to evaluate the operating performance. The numerical wave tank based on the commercial software Fluent 6.2 in the present paper is employed to generate the incident waves. The numerical wave tank consists of the continuity equations, the Reynolds-averaged Navier-Stokes equations and the two-phase VOF function. The oscillating amplitude of water column in the chamber and bi-directional air flow in the duct installed on the top of the chamber are calculated, and compared with experimental data to verify the validation of the present NWT. The nozzle effects of the chamber-duct system on the relative amplitudes of the inner free water surface and air flow rate in the duct are investigated.

Axial Direction Velocity and Wall shear Stress Distributions of Turbulent Steady Flow in a Curved Duct (곡관덕트에 난류정상유동의 축방향 속도분포와 벽면전단응력분포)

  • 이홍구;손현철;이행남;박길문
    • Journal of Advanced Marine Engineering and Technology
    • /
    • v.25 no.1
    • /
    • pp.131-138
    • /
    • 2001
  • In this paper, an experimental investigation of characteristics of developing turbulent steady flows in a square-sectional $180^{\circ}$curved duct is presented. The experimental study using air in a square-sectional $180^{\circ}$ curved duct carryed out to measure axials direction velocity and wall shear stress distrbutions by using Laser Dopper Velocimeter(LDV) system with data acquistion and processing the system of FIND6260 softwere at 7 sections from the inlet($\phi=0^{\circ}$) to the outlet($\phi=180^{\circ}$) in $301^{\circ}$ intervals of a curved duct.

  • PDF

Low Frequency Noise Reduction Inside Duct by Using Membrane (박막을 이용한 저주파수 영역 덕트 소음 저감 방법)

  • 김양한
    • Transactions of the Korean Society for Noise and Vibration Engineering
    • /
    • v.14 no.11
    • /
    • pp.1083-1090
    • /
    • 2004
  • Two noise reduction systems are proposed in order to overcome the geometric restriction of the reactive muffler such as an expansion chamber. First, membrane is installed as a part of a duct wall and an air cavity is covered outside membrane. Second, membrane is installed inside a duct, which gives no volume change of the duct. Structural-acoustic coupling between membrane and fluid inside the cavity and duct causes rapid impedance mismatching and thereby reflected wave. Theoretical prediction is conducted by using modal expansion approach. The results are compared with the experimental results, which show better noise reduction performance than an expansion chamber.

Low frequency noise reduction inside duct by using membrane (박막을 이용한 저주파수 영역 덕트 소음 저감 방법)

  • 전종훈;김양한
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
    • /
    • 2004.05a
    • /
    • pp.474-479
    • /
    • 2004
  • Two noise reduction systems are proposed in order to overcome the geometric restriction of the reactive muffler such as an expansion chamber. First, membrane is installed as a part of a duct wall and an air cavity is covered outside membrane. Second, membrane is installed inside a duct, which gives no volume change of the duct. Structural-acoustic coupling between membrane and fluid inside the cavity and duct causes rapid impedance mismatching and thereby reflected wave. Theoretical prediction is conducted by using modal expansion approach. The results are compared with the experimental results, which show better noise reduction performance than an expansion chamber.

  • PDF

Study of Subsonic Diffusing S-Duct Design Optimization (아음속 확산형 S-덕트 최적 설계에 관한 연구)

  • Kim Su-whan;Kwon Jang-Hyuk
    • 한국전산유체공학회:학술대회논문집
    • /
    • 2002.10a
    • /
    • pp.121-126
    • /
    • 2002
  • Aircraft propulsion systems often use diffusing S-duct to convey air flow from the wing or fuselage intake to the engine compressor, Well designed S-duct should incur minimal total pressure losses and deliver nearly uniform flow with small transverse velocity components at the engine compressor entrance. Reduced total pressure recovery lowers propulsion efficiency and nonuniform flow conditions at the engine face lower engine stall limits. In this study, S-duct which has maximum total pressure recovery and nearly uniform flow profiles at the compressure intake should be found using design optimization methods with 3-dimensional Wavier-Stokes analyses.

  • PDF

Heat Transfer Performance of the Duct with Various Cross Section in Heat Exchanger (단면형상 변화에 따른 전열교환기 열전달 특성변화에 대한 연구)

  • Kim, Eung-Bok;Han, Min-Sub;Kim, Nae-Hyun;Won, Tae-Yeon
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
    • /
    • v.22 no.5
    • /
    • pp.322-327
    • /
    • 2010
  • It is a critical task to keep the ventilation system working in a proper and efficient manner in large multi-storey buildings, and the enthalpy exchanger is becoming an increasingly important part of the ventilation system by playing the function of channeling heat and moisture. We present a computational study on the heat transfer performance of the cross-flow enthalpy exchanger, which is in large use for residential buildings. The ducts are considered whose cross-sectional shapes resemble triangle and longitudinal centerline a cosine wave. It is shown that, as the cross-sectional shape departs from triangle, the heat transfer performance of the duct tends to deteriorate. Also, applying the wave-like shape to the longitudinal centerline of the duct increases the rate of heat transfer and the applied pressure-gradient at the same time. The origin of the performance variations in the cases considered are quantitatively analyzed and discussed.

Flow Characteristics of a Turbulent Pulsating Flow in a Straight Duct Connected to a Curved Duct by using an LDV (LDV에 의한 곡관 후류에 연결된 직관에서 난류맥동유동의 유동특성)

  • 손현철;이행남;박길문
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
    • /
    • v.15 no.3
    • /
    • pp.177-186
    • /
    • 2003
  • In the present study, the flow characteristics of developing turbulent flows are investigated at the exit region of a square cross-sectional 180" curved duct with dimensions of 40mm$\times$40mm$\times$4000mm (height $\times$ width $\times$length). Smoke particles produced from mosquito coils were used as seed particles for the LDV measurement. Experiments were carried out to measure axial velocity profiles, shear stress distributions and entrance lengths by using an LDV system and Rotating Machinery Resolver RMR with PHASE software. Experimental results clearly show that the time-averaged Reynolds number does not affect oscillatory flow characteristics because the turbulent components tend to balance the oscillatory components in the fully developed flow region. Also, the velocity profiles are in good agreement with 1/7power law such as the results of steady turbulent flows. The turbulent intensity linearly increases along the walls and is slightly higher, especially in the period of deceleration. On the other hand, the LDV measurements show that shear stress values in slightly higher in the period of deceleration due to the flow characteristics in the exit region. The entrance length where flows become stable appears at the point that is 40 times the length of hydraulic diameter.eter.

Effects of Discrete Ribs on Pressure Drop in a Rotating Two-Pass Duct (단락요철이 회전덕트 내 압력강하에 미치는 영향)

  • Kim Kyung-Min;Lee Dong-Hyun;Cho Hyung-Hee
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
    • /
    • v.18 no.5
    • /
    • pp.443-450
    • /
    • 2006
  • The present study has been conducted to investigate the effects of rotation on heat/mass transfer and pressure drop characteristics in a two-pass square duct with and without discrete ribs. For stationary cases, the heat/mass transfer on the surfaces with and without discrete ribs is almost the same or reduced. For rotating cases, the gap flow affects differently the heat/mass transfer on leading and trailing surfaces with discrete ribs. On the leading surface of the first pass, the heat/mass transfer is slightly enhanced due to generating strong gap flow. On the trailing surface of the first pass, however, the heat/mass transfer is much decreased because the gap flow disturbs impingement of main flow. The phenomenon, that is, the heat/mass transfer discrepancy between the leading and trailing surfaces is distinctly presented with the increment of rotation number. The friction losses on each surface with discrete ribs are reduced because the blockage ratio decreases for both non-rotating and rotating cases. Therefore, high thermal performance appears in a duct with discrete ribs.

Experiment for Duct Development to Cool Components in Vehicle Engine Room (차량 엔진룸내 부품 냉각용 덕트 개발을 위한 실험)

  • Lee, Suk Young
    • Journal of Energy Engineering
    • /
    • v.27 no.4
    • /
    • pp.98-102
    • /
    • 2018
  • In order to improve the durability of components in the vehicle engine room, an experiment to improve the air cooling effect of components by installing a cooling duct using intake air aiming at four components, such as generator, battery, ECU and power steel oil, Respectively, experimental results show that the overall component temperature has been reduced, and the reduced temperature difference is in the order of generator, ECU, power steel oil and battery. In order to improve the temperature difference due to these components, it is necessary to optimize the design through the flow analysis in the duct in the future.