• 제목/요약/키워드: Turbulence Mode

검색결과 104건 처리시간 0.024초

2차원 표면조도가 있는 난류 평면 Couette-Poiseuille 유동에 대한 직접수치모사 (Turbulent plane Couette-Poiseuille flow over a 2-D rod-roughened wall)

  • 김정현;이영모;이재화
    • 한국가시화정보학회지
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    • 제17권3호
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    • pp.12-18
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    • 2019
  • Direct numerical simulation of a fully developed turbulent plane Couette-Poiseuille flow with a two-dimensional (2-D) rod-roughened wall is performed to investigate the impacts of the surface roughness. It is shown that the logarithmic region in the mean velocity profile over the rough wall Couette-Poiseuille flow is significantly shortened by the surface roughness compared to that over a turbulent Couette-Poiseuille flow with smooth wall. The Reynolds shear stress over the rough wall Couette-Poiseuille flow is decreased compared to that for a smooth case in the outer layer. These results are attributed to weakened turbulence activity or roll-cell mode over the rough wall Couette-Poiseuille flow near the channel centerline due to suppressed development of u'-structure on the top wall, as documented through spanwise energy spectra of the streamwise velocity fluctuations. Inspection of congregation motion near the bottom wall and time evolution of u'-structure reveal weakened co-supporting cycle for the rough wall case.

Convergence Characteristics of Upwind Method for Modified Artificial Compressibility Method

  • Lee, Hyung-Ro;Lee, Seung-Soo
    • International Journal of Aeronautical and Space Sciences
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    • 제12권4호
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    • pp.318-330
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    • 2011
  • This paper investigates the convergence characteristics of the modified artificial compressibility method proposed by Turkel. In particular, a focus is mode on the convergence characteristics due to variation of the preconditioning factor (${\alpha}_u$) and the artificial compressibility (${\beta}$) in conjunction with an upwind method. For the investigations, a code using the modified artificial compressibility is developed. The code solves the axisymmetric incompressible Reynolds averaged Navier-Stokes equations. The cell-centered finite volume method is used in conjunction with Roe's approximate Riemann solver for the inviscid flux, and the central difference discretization is used for the viscous flux. Time marching is accomplished by the approximated factorization-alternate direction implicit method. In addition, Menter's k-${\omega}$ shear stress transport turbulence model is adopted for analysis of turbulent flows. Inviscid, laminar, and turbulent flows are solved to investigate the accuracy of solutions and convergence behavior in the modified artificial compressibility method. The possible reason for loss of robustness of the modified artificial compressibility method with ${\alpha}_u$ >1.0 is given.

Monte Carlo simulation for the response analysis of long-span suspended cables under wind loads

  • Di Paola, M.;Muscolino, G.;Sofi, A.
    • Wind and Structures
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    • 제7권2호
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    • pp.107-130
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    • 2004
  • This paper presents a time-domain approach for analyzing nonlinear random vibrations of long-span suspended cables under transversal wind. A consistent continuous model of the cable, fully accounting for geometrical nonlinearities inherent in cable behavior, is adopted. The effects of spatial correlation are properly included by modeling wind velocity fluctuation as a random function of time and of a single spatial variable ranging over cable span, namely as a one-variate bi-dimensional (1V-2D) random field. Within the context of a Galerkin's discretization of the equations governing cable motion, a very efficient Monte Carlo-based technique for second-order analysis of the response is proposed. This procedure starts by generating sample functions of the generalized aerodynamic loads by using the spectral decomposition of the cross-power spectral density function of wind turbulence field. Relying on the physical meaning of both the spectral properties of wind velocity fluctuation and the mode shapes of the vibrating cable, the computational efficiency is greatly enhanced by applying a truncation procedure according to which just the first few significant loading and structural modal contributions are retained.

무인 헬기 자동 착륙을 위한 3차원 위치 추적 시스템 (Three-Dimensional Location Tracking System for Automatic Landing of an Unmanned Helicopter)

  • 추영열;강성호
    • 제어로봇시스템학회논문지
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    • 제14권6호
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    • pp.608-614
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    • 2008
  • This paper describes a location tracking system to guide landing process of an Unmanned Helicopter(UMH) exploiting MIT Cricket nodes. For automatic landing of a UMH, a precise positioning system is indispensable. However, GPS(Global Positioning System) is inadequate for tracking the three dimensional position of a UMH because of large positioning errors. The Cricket systems use Time-Difference-of-Arrival(TDoA) method with ultrasonic and RF(Radio Frequency) signals to measure distances. They operate in passive mode in that a listener attached to a moving device receives distance signals from several beacons located at fixed points on ground. Inevitably, this passive type of implementation causes large disturbances in measuring distances between beacons and the listener due to wind blow from propeller and turbulence of UMH body. To cope with this problem, we proposed active type of implementation for positioning a UMH. In this implementation, a beacon is set up at UMH body and four listeners are located at ground area at least where the UMH will land. A pair of Ultrasonic and RF signals from the beacon arrives at several listeners to calculate the position of the UMH. The distance signals among listeners are synchronized with a counter value appended to each distance signals from the beacon.

Use of laminar flow water storage tank (LFWS) to mitigate the membrane fouling for reuse of wastewater from wafer processes

  • Sun, Darren Delai;Wu, You
    • Membrane and Water Treatment
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    • 제3권4호
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    • pp.221-230
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    • 2012
  • This study employed the modified fouling index (MFI) to determine the performance of a two-step recycling system - a membrane filtration integrated laminar flow water storage (LFWS) tank followed by an ion exchange process to reclaim ultrapure water (UPW) from the wastewater generated from semiconductor wafer backgrinding and sawing processes. The first step consisted of the utilization of either ultrafiltration (UF) or nanofiltration (NF) membranes to remove solids in the wastewater where the second step consisted of an ion exchanger to further purify the filtrate. The system was able to produce high purity water in a continuous operating mode. However, higher recycling cost could be incurred due to membrane fouling. The feed wastewater used for this study contained high concentration of fine particles with low organic and ionic contents, hence membrane fouling was mainly attributed to particulate deposition and cake formation. Based on the MFI results, a LFWS tank that was equipped with a turbulence reducer with a pair of auto-valves was developed and found effective in minimizing fouling by discharging concentrated wastewater prior to any membrane filtration. By comparing flux behaviors of the improved system with the conventional system, the former maintained a high flux than the latter at the end of the experiment.

이중목 노즐 개념에 기반한 유체 추력벡터제어에 관한 연구 (Study on Fluidic Thrust Vector Control Based on Dual-Throat Concept)

  • ;김희동
    • 한국추진공학회지
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    • 제23권1호
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    • pp.24-32
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    • 2019
  • 유체 추력벡터 제어에서 이중목 노즐 개념의 이용 가능성을 조사하기 위하여, 초음속 노즐에서 수치해석을 수행하였다. 수치해석 검증에서 SST $k-{\omega}$ 난류모델을 사용하여 실험결과를 잘 구현하였다. 광범위한 노즐 압력비와 분사 압력비에서 편향각도, 시스템의 전체 추력비 및 추력 효율을 조사하였다. 본 연구에서 이중목 노즐의 추력벡터제어 시스템의 성능 변화는 2차원 계산영역에서 명확하게 설명되었다. 본 연구에서 얻어진 결과들은 유체추력벡터제어 분야에 중요한 기초자료를 제공할 것이다.

Loss Analysis by Impeller Blade Angle in the S-Curve Region of Low Specific Speed Pump Turbine

  • Ujjwal Shrestha;Young-Do Choi
    • 신재생에너지
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    • 제20권2호
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    • pp.35-43
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    • 2024
  • A pump turbine is a technically matured option for energy production and storage systems. At the off-design operating range, the pump turbine succumbed to flow instabilities, which correlated with the pump turbine geometry. A low specific speed pump turbine was designed and modified according to the impeller blade angle. Reynolds-Average Navier-Stokes is carried out with a shear stress transport turbulence model to evaluate the detailed flow characteristics in the pump turbine. The impeller blade inlet angle (𝛽1) and outlet angle (𝛽2) are used to evaluate hydraulic loss in the pump turbine. When 𝛽1 changed from low to high value, the maximum efficiency is increased by 4.75% in turbine mode. The S-Curve inclination is reduced by 8% and 42% for changes in 𝛽1 and 𝛽2 from low to high values, respectively. At α = 21°, the shock loss coefficient (𝜁s) is reduced by 16% and 19% with increases of 𝛽1 and 𝛽2 from low to high values, respectively. When 𝛽1 and 𝛽2 values increased from low to high, the impeller friction coefficient (𝜁f) increased and decreased by 20% and 8%, respectively. Hence, the high 𝛽2 effectively reduced the loss coefficient and S-Curve inclination.

경사충격파와 와류간의 상호작용에 관한 수치적 연구 (A numerical investigation on the oblique shock wave/vortex interaction)

  • 문성목;김종암;노오현;홍승규
    • 한국항공우주학회지
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    • 제32권8호
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    • pp.20-28
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    • 2004
  • 경사충격파와 와류간의 상호작용에 관한 수치적 해석은 경사충격파에 기인한 와류붕괴 의 발생에 관한 이론적 모델 및 실험치와 비교하기 위해 수행되었다. 본 연구의 해석을 위해 마하수에 기초한 Roe의 기법 (RoeM) 과 2-방정식 난류 모델을 이용하여 3차원 난류 유동장을 효과적으로 계산하였다. 자유류 마하수 2.49에서 와유세기, 축방향속도 성분, 충격파 세기의 변화에 따른 상호작용의 영향을 연구하였다. 2-방정식 난류모델인 k-wSST 난류모델과 적절히 모델링된 와류모델을 이용하여 수치연구를 수행함으로써 실험적으로 관찰된 여러 유동장을 정확히 모사할 수 있었다. 경사충격파에 기인한 와류붕괴의 발생에 관한 기준을 결정하기 위한 본 연구결과는 이론적 모델과 실험치와 일치된 결과를 보여주고 있음을 확인하였다.

POD와 DMD를 이용한 와류형 분사기의 극저온 질소 분무 동적 특성 분석 (Dynamic Characteristics Analysis of the Cryogenic Nitrogen Injection of Swirl Injector using POD and DMD)

  • 강정석;성홍계;손채훈
    • 한국추진공학회지
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    • 제21권5호
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    • pp.1-9
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    • 2017
  • 초임계 환경에서 와류형 분사기의 극저온 질소 분무 동적 특성 분석을 위하여 3차원 LES 난류 모델을 적용하였다. 초임계 상태에서 질소의 상태량들을 정확하게 예측하기 위해 SRK 실기체 상태방정식을 사용하였고, 점성계수와 열전도도는 Chung의 고압 상태 혼합물에 대한 방정식, 그리고 확산 계수는 Fuller의 이론에 Takahashi의 보정식을 적용하였다. 질소 분무 결과, 분사기 내, 외부에서 유동장과 음향장 사이의 상호작용으로 복잡한 유동구조가 형성된다. 복잡한 유동 현상을 분석하기 위해 FFT, POD 그리고 DMD 기법을 적용하여 해석을 수행하였다. FFT 해석을 수행하여 분사기 내, 외부에서 나타나는 특정 주파수를 파악하였으며, POD와 DMD를 통해 각 주파수가 어떠한 유동 구조를 갖는지에 대한 연구를 수행하였다. 또한, DMD를 통해 각 주파수의 감쇠 계수를 파악하여 이를 실험 결과와 비교하였다.

PAGAN I: MULTI-FREQUENCY POLARIMETRY OF AGN JETS WITH KVN

  • KIM, JAE-YOUNG;TRIPPE, SASCHA;SOHN, BONG WON;OH, JUNGHWAN;PARK, JONG-HO;LEE, SANG-SUNG;LEE, TAESEOK;KIM, DAEWON
    • 천문학회지
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    • 제48권5호
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    • pp.285-298
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    • 2015
  • Active Galactic Nuclei (AGN) with bright radio jets offer the opportunity to study the structure of and physical conditions in relativistic outflows. For such studies, multi-frequency polarimetric very long baseline interferometric (VLBI) observations are important as they directly probe particle densities, magnetic field geometries, and several other parameters. We present results from first-epoch data obtained by the Korean VLBI Network (KVN) within the frame of the Plasma Physics of Active Galactic Nuclei (PAGaN) project. We observed seven radio-bright nearby AGN at frequencies of 22, 43, 86, and 129 GHz in dual polarization mode. Our observations constrain apparent brightness temperatures of jet components and radio cores in our sample to > 108.01 K and > 109.86 K, respectively. Degrees of linear polarization mL are relatively low overall: less than 10%. This indicates suppression of polarization by strong turbulence in the jets. We found an exceptionally high degree of polarization in a jet component of BL Lac at 43 GHz, with mL ~ 40%. Assuming a transverse shock front propagating downstream along the jet, the shock front being almost parallel to the line of sight can explain the high degree of polarization.