• 제목/요약/키워드: Unsteady Periodic Flow

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초음속난류유동장에서 후향계단 후류의 측면제트분사에 대한 수치적 연구 (Numerical Study of slot injection behind a rearward-facing step into turbulent supersonic flow)

  • 김종록;김재수
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2002년도 춘계 학술대회논문집
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    • pp.17-22
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    • 2002
  • This paper describes numerical research on transverse jet behind rearward-facing step in turbulent supersonic flowfields without chemical reaction. The purpose of transverse jet behind rearward-facing step is to improve mixing of the fuel in the combustor. Two-dimensional unsteady flowfields generated by slot injection into supersonic flow are numerically simulated by integration of Navier-Stokes equation. Final-scale turbulence effects are modeled with two-equation $\kappa-\epsilon$ model. Numerical methods are modeled high-order upwind TVDschemes. A total of 4 cases are computed, comprising slot momentum flux ratios at four step heights downstream of the step. These numerical results are represented periodic phenomenon in unsteady flowfields.

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원관내 왕복유동에서 비정상 열전달 관계식의 공식화 (A new formulation for unsteady heat transfer of oscillatory flow in a circular tube)

  • 박상진;이대영;노승탁
    • 대한기계학회논문집B
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    • 제20권9호
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    • pp.2953-2964
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    • 1996
  • 왕복유동에 의한 순간 열전달현상은, 왕복유동의 두가지 특성인 왕복주파수와 왕복거리를 나타내는 .betha.와 .gamma.에 의하여 결정되고, 그 특성에 따라 세영역으로 나누어짐을 확인하였다. 영역 I에서는 일방향유동에서와 마찬가지로 열유속이 평균온도차에 비례하고, 영역 II에서는 열유속과 평균온도차간에 약 45.deg.의 위상차가 발생하지만 모두 1차 조화성분이 주로 나타났다. 한편 영역 III의 경우에는 위상차가 생길뿐만 아니라 평균온도차에 고차 조화성분이 나타났다. 기존의 방법인 복소 Nusselt수를 고차 조화성분까지 확장하면 열유속을 평균온도차로 나타낼 수 있지만 각 조화성분의 정보를 다 알아야하므로 실제 적용이 불가능하였다.

An Experimental Investigation of Unsteady Mixed Convection in a Horizontal Channel with Cavity Using Thermo-Sensitive Liquid Crystals

  • Bae, Dae-Seok;Cai, Long-Ji;Kim, Eun-Pil
    • Journal of Advanced Marine Engineering and Technology
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    • 제33권7호
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    • pp.987-993
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    • 2009
  • An experimental study is performed to investigate unsteady mixed convection in a horizontal channel with a heat source. Particle image velocimetry (PIV) with thermo-sensitive liquid crystal (TLC) tracers is used for visualization and analysis. This method allows simultaneous measurement of velocity and temperature fields at a given instant of time. Quantitative data of the temperature and velocity are obtained by applying the color-image processing to a visualized image, and neural network is applied to the color-to-temperature calibration. It is found that the periodic flow of mixed convection in a cavity appears at very low Reynolds numbers (Re<0.4), and the period decreases with increasing Reynolds numbers and increases with increasing aspect ratio.

정방형 벨트구동 캐비티의 흐름특성에 관한 연구 (A Study on Flow Characteristics of Lid-Driven Square Cavity)

  • 김진구;조대환;김춘식;이영호
    • Journal of Advanced Marine Engineering and Technology
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    • 제21권4호
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    • pp.430-436
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    • 1997
  • Time-dependent Flow characteristics of a two-dimensional lid-driven square cavity flow of six high Reynolds numbers, $10^4 2{\times}lO^4., 3{\times}l0^4, 5{\times}lO^4, 7.5{\times}lO^4$ and $10^5$ were investigated. A convection conservative difference scheme based upon SOLA to maintain the nearly 2nd-order spatial accuracy was adopted on irregular grid formation. Irregular grid number is $80{\times}80$ and its minimum size is about 1/400 of the cavity height(H) and its maximum is about 1/53 H. The result shows that at Re= $10^4$, periodic migration of small eddies appearing in corner separation region and its temporal sinusoidal fluctuation are represented. And another critical Reynolds number which shows the commencement of flow randomness emerging from the periodic fluctuation is assumed to be around Re= $1.5{\times}10$. At five higher Reynolds numbers ($2{\times}lO^4., 3{\times}l0^4, 5{\times}lO^4, 7.5{\times}lO^4$ and $10^5$), an organizing structure of four consecutive vortices similar to a Moffat vortex at two lower corners is revealed from time-mean flow patterns.

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전향 스윕 프로펠러 홴의 성능 및 유동특성 (Performance and Flow Characteristics of a Forward Swept Propeller Fan)

  • 김진권;강신형
    • 대한기계학회논문집B
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    • 제24권1호
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    • pp.75-84
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    • 2000
  • Performance and flow characteristics of a small forward swept propeller fan for home refrigerators are studied experimentally. An unusual discontinuity is observed in the performance curve of the fan. Mean flow fields measured with as-hole Pitot probe reveal that the flow is axial at the high flow rate and radial at the low flow rate. The flow structure changes abruptly across the discontinuity. Unsteady flow measurements with a set of hot-wire probes indicate that near the discontinuity a single-cell stall rotates at 40% speed of the fan speed, while away from the discontinuity the flow shows periodic variation corresponding to the blade passage frequency. Phase-lock averaged flow fields measured with a triple-sensor hot-wire probe show that there appears radially inward flow over the pressure side of the blade and the outward passage flow over the tip.

측면제트분사가 있는 후향계단 후류의 비정상초음속유동에 대한 수치적 연구 (Numerical Study of Unsteady Supersonic Flow Behind a Rearward-Facing Step with Slot Injection)

  • 김종록;김재수
    • 한국항공우주학회지
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    • 제31권1호
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    • pp.97-103
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    • 2003
  • 연소기 내부에서 연소효율의 증대목적으로 사용되어지고 있는 후향계단후류의 측면제트 분사가 있는 초음속 난류유동장에 대한 수치적 연구를 수행하였다. 본 연구에서는 2차원 Navier_Stokes 방정식과 k-$\varepsilon$ 난류모델식을 고해상도 풍상차분법인 TVD 기법을 사용하여 비정상 유동장에 대한 수치계산을 수행하였다. 유동특성은 제트분사에 의한 마하면이 장애물 역할을 하여 후향계단과 마하면사이에 공동유동(cavity flow)과 비슷한 유동현상이 나타난다. 따라서, 공동 유동에서 발생하는 유동의 진동특성이 나타날 것을 예측할 수 있다. 수치계산 결과에서도 모맨텀플럭스와 분사위치에 따라, 공동유동에서 발생하는 진동특성을 갖는 비정상 유동 특성이 나타나는 것을 볼 수 있었다.

대각 내재적 조화균형법을 이용한 헬리콥터 로터 블레이드의 비정상 공력 해석 (UNSTEADY AERODYNAMIC ANALYSIS OF HELICOPTER ROTOR BLADES USING DIAGONAL IMPLICIT HARMONIC BALANCE METHOD)

  • 임동균;최성임;박수형;권장혁
    • 한국전산유체공학회지
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    • 제16권4호
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    • pp.21-27
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    • 2011
  • In this paper, the diagonal implicit harmonic balance method is applied to analyze helicopter rotor blade flow. The periodic boundary condition for Fourier coefficients is also applied in hover and forward flight conditions. It is available enough to simulate the forward flight problem with only one rotor blade using the periodic boundary condition in the frequency domain. In order to demonstrate the present method, Caradonna & Tung's rotor blades were used and the results were compared to the time-accurate method and experimental data.

대각 내재적 조화균형법을 이용한 헬리콥터 로터 블레이드의 비정상 공력 해석 (Unsteady Aerodynamic Analysis of Helicopter Rotor Blades Using Diagonal Implicit Harmonic Balance Method)

  • 임동균;최성임;박수형;권장혁
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2011년 춘계학술대회논문집
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    • pp.543-549
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    • 2011
  • In this paper, diagonal implicit harmonic balance method is applied to analyze helicopter rotor blade flow. Periodic boundary condition for Fourier coefficients is also applied in hover and forward flight condition. It is available enough to simulate the forward flight problem with only one rotor blade using the periodic boundary condition in frequency domain. In order to demonstrate present method Carodonna & Tung's rotor blades are used and the results are compared to time-accurate method and experimental data.

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간헐 열전달을 이용한 밀폐용기내의 물질전달 향상 (Enhancement of Mass Transfer of an Enclosed Fluid by Time-periodic Thermal Forcing)

  • 곽호상
    • 한국전산유체공학회지
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    • 제7권1호
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    • pp.36-43
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    • 2002
  • A numerical investigation is made of unsteady double-diffusive convection of a Boussinesq fluid in a rectangular cavity subject to time-periodic thermal excitations. The fluid is initially stratified between the top endwall of low solute concentration and the bottom endwall of high solute concentration. A time-dependent heat flux varying in a square wave fashion, is applied on one sidewall to induce buoyant convection. The influences of the imposed periodicity on double-diffusive convection are examined. A special concern is on the occurrence of resonance that the fluctuations of flow and attendant heat and mass transfers are mostly amplified at certain eigenmodes of the fluid system. Numerical solutions illustrate that resonant convection results in a conspicuous enhancement of time-mean mass transfer rate.

Numerical investigation of supercavity geometry and gas leakage behavior for the ventilated supercavities with the twin-vortex and the re-entrant jet modes

  • Xu, Haiyu;Luo, Kai;Dang, Jianjun;Li, Daijin;Huang, Chuang
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제13권1호
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    • pp.628-640
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    • 2021
  • To investigate the supercavity geometry and gas flow structure for the supercavities with two closure types under the different flow conditions, an inhomogeneous multiphase model with the SST turbulence model was established, and validated by experimental results. The results show that two distinct regions exist inside the supercavity, which include the downstream flow region along the gas-water interface and the reverse flow region. For the twin-vortex supercavity, the internal gas leaks from the supercavity boundary by two paths: the supercavity surface and the two-vortex tubes. Increasing Froude number leads to more internal gas stripped from the supercavity surface. Two types of gas loss exist for the re-entrant jet supercavity with high Froude number, one type is the steady process of gas loss, and the major gas-leaking path is the supercavity surface rather than supercavity closure region. The other type is the unsteady periodic ejection, and the gas cluster of periodic ejection is merely a small part of the gas stored inside the supercavity.