• 제목/요약/키워드: 후향 계단

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수정 난류모델에 의한 후향계단 유동예측 (Prediction of a Backward-Facing Step Flow with Modified Turbulence Models)

  • 명현국;백인철;한화택
    • 대한기계학회논문집
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    • 제18권11호
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    • pp.3039-3045
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    • 1994
  • The k-$\varepsilon$ turbulence models by Launder et al.(1977, LPS) and Leschziner and Rodi(1981, LR) are modified to account for the secondary straining effect with having a generality in the present paper. The modified models are obtained by replacing the gradient Richardson number used to account for the secondary straining effect in the original models by a new parameter with a tensor-invariant correction form. These two modified models are used to predict the turbulent flow over a backward-facing step. In contrast to both standard and modified LR models, the modified LPS model is found to predict the reattachment point fairy well, as well as mean velocity, wall static pressure, turbulent kinetic energy and Reynolds shear stress in the recirculating region.

CFD에 의한 2차원 후향계단에서의 재부착 유동특성에 관한 연구 (A Study on Flow Characteristics of Two-Dimensional Backward-Facing Step by CFD)

  • 최영도;이영호
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 1998년도 추계 학술대회논문집
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    • pp.127-132
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    • 1998
  • The present study is aimed to investigate flow characteristics of Two dimensional backward-facing step by numerical approach. A convection conservative difference scheme based upon SOLA algorithm is used for the solution of the two-dimensional incompressible Navier-Stokes equations to simulate the laminar, transitional and turbulent flow conditions at which the experimental data can be available for the backward-facing step. The twenty kinds of Reynolds number are used for the calculations. In an effort to demonstrate that the reported solutions are dependent on the mesh refinement, computations are performed on seven different meshes of uniformly increasing refinement. Also to investigate the result of inflow dependence, two kinds of the inflow profile are chosen for the laminar flow. As criterion of benchmarking the result of numerical simulation, reattachment length is used for the selected Reynolds numbers.

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자유흐름 난류강도가 후향계단유동에 미치는 영향에 대한 실험 (An Experiment on the Effects of Free Stream Turbulence Intensity on the Backward-Facing Step Flow)

  • 김사량;유정열
    • 대한기계학회논문집
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    • 제19권9호
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    • pp.2297-2307
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    • 1995
  • An experimental study on the structure of a separated shear layer downstream of the backward-facing step has been performed by examining mean flow and turbulent quantities in terms of free stream turbulence. When free stream turbulence exists, the entrainment rate of the separated shear layer and the flow rate in the recirculation region are enhanced, resulting in shorter reattachment length. The production and diffusion terms in the turbulent kinetic energy balance are shown to increase more than the dissipation term does. Rapid decrease of the pressure-strain term in the shear stress balance implies the enhancement of the three-dimensional motion by free stream turbulence.

후향계단을 지나는 박리류에 대한 레이놀즈응력 모델의 성능 평가 (Assessment of Reynolds Stress Turbulence Closures for Separated Flow over Backward-Facing Step)

  • 김광용;오명택
    • 대한기계학회논문집
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    • 제19권11호
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    • pp.3014-3021
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    • 1995
  • This study is carried out in order to evaluate the performances of the Reynolds stress turbulence models such as SSG and GL models in the calculation of separated flow over backward-facing stepp.In addition, two slow return-to-isotropy models, YA and Rotta models combined with rapid part of SSG model are also tested. The finite volume method is used to discretize the governing differential equations, and the power-law scheme is used to approximate the convection terms. The SIMPLE algorithm is used for pressure correction in the governing equations. The results show that SSG model gives the better prediction near the reattachment point than GL model. In cases that the rapid term of SSG model is combined with Rotta and YA slow models, the results show the better predictions of stress components in recirculation zone, but indicate inaccuracy in the predictions of mean velocity.

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

  • 안상훈;한두희;최한영;서성현;성홍계
    • 항공우주시스템공학회지
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    • 제13권6호
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    • pp.9-16
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    • 2019
  • 초음속 유동이 흐르는 후향 계단에서 액체 제트가 수직으로 분사되는 유동의 혼합 특성에 대한 실험적 연구를 수행하였다. 작동 유체는 질소와 물을 사용하였다. 쉐도우그래프 기법을 사용하여 유동을 가시화하였으며, 초고속 카메라로 촬영된 영상은 시간 평균화 처리를 통해 분석에 사용하였다. 액체 제트의 주입구는 초음속 질소가스 유동에 의해 생성되는 재순환 영역 내부에 위치하며 유동방향에 수직하게 분사된다. 실험 조건은 질소가스 챔버와 액체 가압탱크의 압력에 따라 나누었다. 각 실험 조건에서 분사된 액체 제트의 침투 깊이와 마하 디스크의 생성 위치의 변화를 관찰하였으며, 운동량비에 따른 유동의 구조 변화에 대해 고찰하였다.

슬롯 분사가 있는 후향계단 유동장 분석을 위한 초음속풍동 설계 (Design of Supersonic Wind Tunnel for Analysis of Flow over a Backward Facing Step with Slot Injection)

  • 김익태
    • 한국산학기술학회논문지
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    • 제17권11호
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    • pp.363-367
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    • 2016
  • 본 연구는 마하수 2.5의 초음속 영역에서 마하수 1.0의 슬롯 분사가 있는 후향계단 형상에 대한 유동장 특성을 분석하기 위하여 초음속풍동 시험부를 설계, 제작하였다. 비행체가 고속으로 움직일 때 공동 주위의 유동은 매우 복잡하여 수치해석 결과를 검증할 초음속풍동 시험 자료가 필요하기 때문에 기존의 2차원 대칭형 노즐을 아랫면이 평판인 비대칭형 노즐로 수정하였다. 특성곡선해법을 이용한 비점성 노즐을 설계하고, 시험을 통해 얻은 경계층 두께를 노즐에 반영하여 보정한 기법을 C 언어로 프로그래밍하여 얻은 결과를 수치해석 결과와 비교하여 검증하였다. 슬롯 분사 시 지속적인 유동장 변화 분석을 위한 초음속 유지시간 확보를 위해 저장탱크의 압력 변화에 따른 PID 제어프로그램 수정으로 초음속 유동 유지시간을 약 5초에서 약 6초로 1초 정도 연장하여 제어 효율을 향상하였고, 슬롯 분사가 있는 후향계단에서의 유동장 변화를 슐리렌장치로 가시화하여 복잡한 유동장 특성을 확인하였다. 향후 슬롯 분사의 속도와 유량, 유동장의 온도를 변화하여 공동에서의 막냉각 효과 분석을 위한 장비로 사용할 계획이다.

후향 계단 주위 난류 박리 유동에 대한 비정상 후류의 영향 (Influence of Unsteady Wake on Turbulent Separated Flows over a Backward-Facing Step)

  • 전세종;성형진
    • 대한기계학회논문집B
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    • 제27권12호
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    • pp.1708-1715
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    • 2003
  • An experimental study was made of turbulent separated and reattaching flow over a backward-facing step, where unsteady wake was generated by a spoked-wheel type wake generator with cylindrical rods in front of the separated flow. The influence of unsteady wake was scrutinized in terms of the rotating speed of the wake generator (0$\leq$S $t_{H}$$\leq$0.4). A conditional averaging technique in corporation with SBF was employed to elucidate the influence of the unsteady wake on the large-scale vortical structures of the separated flow. Special attention was made during two-dimensional measurements of wall-pressure with or without unsteady wake. The wall-pressure fluctuations were used to predict dipole sound source by Curie's integral formula. It was found that the reduction of the dipole sound source was due to the reduction of turbulent kinetic energy by unsteady wake in the recirculation region.n.

조도가 후향계단 주위의 난류유동에 미치는 영향에 대한 실험적 연구 (An Experimental Study of Roughness Effects on the Turbulent Flow Downstream of a Backward-Facing Step)

  • 김병남;정명균
    • 대한기계학회논문집
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    • 제15권6호
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    • pp.2083-2099
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    • 1991
  • 본 연구에서는 다른 실험 조건은 일정하게 유지하면서 아래 벽면의 표면조도 를 체계적으로 변화시켜 표면조도가 후향계단 뒤의 재부착 흐름 및 재발달경계층에 미 치는 영향을 조사하고자 하며 구체적인 내응은 다음과 같다. (1) 표면조도가 재부착 길이와 재발달경계층에 미치는 영향의 조사. (2) 표면조도가 평균속도와 난류량 분포 에 미치는 영향의 조사. (3) 여러 종류 표면조도 변화에 따른 재부착길이와 재발달 경 계층 회복에 미치는 영향과 결과의 상호 비교.

후향계단 DDES 해석의 길이척도 영향 분석 (EFFECT OF LENGTH-SCALE IN DDES FOR BACKWARD-FACING STEP FLOW)

  • 이충연;사정환;박수형;이은석;이진익;이광섭
    • 한국전산유체공학회지
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    • 제17권4호
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    • pp.24-31
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    • 2012
  • Effects of the subgrid length-scale in the Delayed-Detached Eddy Simulation(DDES) are investigated based on the Spalart-Allmaras(S-A) and the k-$\omega$ Shear Stress Transport(SST) turbulence models. Driver & Seegmiller's experimental results are used to validate numerical results. Grid convergence with grid resolution and subgrid length-scale is investigated. The simulation results show that the volume method for the subgrid length-scale is more resistant to unfavorable effects of the grid size in the periodic direction than the maximum method. Using a sufficient grid resolution and an appropriate subgrid length-scale, both S-A based DDES and SST based DDES methods can provide a good correlation with the experimental data.

후향계단 난류 박리재부착 유동에서의 대형와의 구조 (Large-Scale Vertical Structure in Separated and Reattaching Turbulent flow over a Backward Facing Step)

  • 안승광;이인원;성형진
    • 대한기계학회논문집B
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    • 제26권12호
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    • pp.1674-1680
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    • 2002
  • An experimental study was made of a large-scale vortical structure over a backward-facing step. The Reynolds number based on the step height was R $e_{H}$ =33,000. To recognize the large-scale vortex, three components of velocity were measured. The measurements were performed in the recirculation zone (x/H=4.0) and the reattachment zone(x/H=7.5). To measure the wall pressure fluctuations in a turbulent flow over a backward-facing step, a 32-channel microphone array was installed beneath the wall in the streamwise and spanwise directions. From the measured pressure field, the size of large-scale vortex was obtained. As a detailed study, a conditionally-averaging technique was employed to characterize the coherent structure of the large-scale vortex. To see the relationship between the flow field and the relevant spatial mode of the pressure field, the spatial box filtering (SBF) was examined. A cross-correlation between velocity and pressure fluctuations was performed to identify the structure and the length scale of the large-scale vortex.x.