• Title/Summary/Keyword: Parallel flow field

Search Result 157, Processing Time 0.038 seconds

A NOTE ON THE UNSTEADY FLOW OF DUSTY VISCOUS FLUID BETWEEN TWO PARALLEL PLATES

  • AJADI SURAJU OLUSEGUN
    • Journal of applied mathematics & informatics
    • /
    • v.18 no.1_2
    • /
    • pp.393-403
    • /
    • 2005
  • We study the isothermal flow of a dusty viscous incompressible conducting fluid between two types of boundary motions- oscillatory and non-oscillatory, under the influence of gravitational force. Within the frame work of some physically realistic approximations and suitable boundary conditions, closed form solutions were obtained for the velocity profiles and the skin friction of the particulate flow. These results show that for a constant pressure gradient, only the velocity profile of the fluid and the skin friction are unaffected by gravity, while magnetic field is seen to affect both the fluid, particle velocities and the skin friction. Thus, our results are extension of previous results in literature, and graphical demonstration of some these solutions have been presented.

A Fluid Flow Numerical Study on the Design Factor of Inlet Distribution Channel for Flocculation/Sedimentation Basin (유동(流動) 수치해석(數値解析)을 이용한 응집·침전지 유입 분배수로 설계인자 연구)

  • Yoon, Jang-Ken;Kim, Jeong-Hyun;Oh, Jung-Woo;Ha, Eun-Jung
    • Journal of Korean Society of Water and Wastewater
    • /
    • v.14 no.4
    • /
    • pp.337-342
    • /
    • 2000
  • In water treatment plants, open channel is used to distribute incoming flow to parallel treatment unit, such as flocculation basin and sedimentation basin. These control devices must be designed so that the incoming flow evenly distributed to the process unit. this is important in the view of optimizing process unit. In the recent past. significant insights into the sedimentation process have been developed. In this study, the 2-D computer program is developed to investigate fluid flow field and velocity vectors in flocculation sedimentation inlet distribution weir and calculate flow rates in each inlet weir. The specific purpose of this study is to analyze physical design factors, such as now rates, shape of channel, tapered angle in tapered type channel and main channel width.

  • PDF

Study on Fluid Flow and Thermal Characteristics in a Nanoscale Channel Using MD Simulation (분자 동역학 시뮬레이션을 이용한 나노 스케일 채널 내에서의 유체 유동 및 열적 특성에 관한 연구)

  • Choi, Yong-Seok;Kim, Sung-Jin
    • Proceedings of the KSME Conference
    • /
    • 2004.04a
    • /
    • pp.1880-1884
    • /
    • 2004
  • To analyze the fluid flow and thermal characteristics in a nanoscale system, the planar Poiseuille flow of a Lennar-Jones liquid through parallel plates formed by fixed atoms is studied using nonequilibrium molecular dynamics simulations. The role of important simulation parameters such as the channel width, the magnitude of external field, the temperatures of the top and bottom plates, and the interaction potential parameter between fluid and wall atoms, which affect flow patterns and heat transfer rate inside the channel, are investigated. Under the various simulation conditions, interesting phenomena deviated from the continuum predictions have found.

  • PDF

A Numerical Study of Blade Sweep Effect in Supersonic Turbine Rotor (초음속 터빈의 로터 블레이드 스윕 효과에 대한 수치적 연구)

  • Jeong, Soo-In;Jeong, Eun-Hwan;Kim, Kui-Soon
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2011.11a
    • /
    • pp.830-834
    • /
    • 2011
  • In this study, we performed three-dimensional CFD analysis to investigate the effect of the rotor blade sweep of a partial admission supersonic turbine on the stage performance and the flow field. The computations are conducted for three different sweep cases, No sweep(NSW), Backward sweep(BSW), and Forward sweep(FSW), using flow analysis program, $FLUENT^{TM}$ 6.3 Parallel. The results show that BSW model give the effect on the reducing of mass flow rates of tip leakage and the increasing of t-to-s efficiency.

  • PDF

A Numerical Study on the Performance Characteristics of a Partial Admission Axial Supersonic Turbine with Swept Rotor Blades (로터 블레이드 스윕을 적용한 부분흡입형 축류 초음속 터빈의 성능특성에 대한 수치적 연구)

  • Jeong, Sooin;Kim, Kuisoon
    • Journal of the Korean Society of Propulsion Engineers
    • /
    • v.17 no.3
    • /
    • pp.1-8
    • /
    • 2013
  • In this study, we performed three-dimensional CFD analysis to investigate the effect of the rotor blade sweep of a partial admission supersonic turbine on the stage performance and the flow field. The computations are conducted for three different sweep cases, No sweep(NSW), Backward sweep(BSW), and Forward sweep(FSW), using flow analysis program, FLUENT 6.3 Parallel. The results of the BSW model show reduced mass flow rates of tip leakage and increased total-to-static efficiency. The strength of leading edge bow shock was decreased a little with BSW model. And the BSW model also shows a good performance around the hub region compared to other models.

Spiral Magnetic Field Lines in a Hub-Filament Structure, Monoceros R2

  • Hwang, Jihye;Kim, Jongsoo
    • The Bulletin of The Korean Astronomical Society
    • /
    • v.45 no.1
    • /
    • pp.59.3-60
    • /
    • 2020
  • We present the results of polarization observations at submillimeter wavelengths towards Monoceros R2 (Mon R2). The polarized thermal dust emission was obtained from SCUBA-2/POL-2 at 450 ㎛ and 850 ㎛, simultaneously. This observation is a part of the JCMT BISTRO survey project. The polarization angle distributions at 450 ㎛ and 850 ㎛ are similar and the mean value of angle differences at two wavelengths is 5.5 degrees. The Mon R2 is one of massive star-forming regions containing a clear hub-filamentary structure. The hub region shows star formation activities, and surrounding filaments provide channels for matters to move into the hub region. It is not well known the role of magnetic fields in a hub-filamentary structure. Some studies have shown well-ordered polarization segments along a filamentary structure and magnetic field morphology traced by polarization segments is interpreted as to help gas flow along the filamentary structrue. Our observations shows that filaments in Mon R2 have spiral structure and the magnetic field lines are parallel to the filaments. We interpret that the spiral structure can be formed by a rotation hub-filament system with gas flowing along the filaments to the hub. We found several dust clumps at the central part of the hub region of the Mon R2. They seems to be formed at locations where spiral field lines meet each other. These results show one observational example that a magnetic field play a role in gas flow.

  • PDF

Resource and Delay Efficient Polynomial Multiplier over Finite Fields GF (2m) (유한체상의 자원과 시간에 효율적인 다항식 곱셈기)

  • Lee, Keonjik
    • Journal of Korea Society of Digital Industry and Information Management
    • /
    • v.16 no.2
    • /
    • pp.1-9
    • /
    • 2020
  • Many cryptographic and error control coding algorithms rely on finite field GF(2m) arithmetic. Hardware implementation of these algorithms needs an efficient realization of finite field arithmetic operations. Finite field multiplication is complicated among the basic operations, and it is employed in field exponentiation and division operations. Various algorithms and architectures are proposed in the literature for hardware implementation of finite field multiplication to achieve a reduction in area and delay. In this paper, a low area and delay efficient semi-systolic multiplier over finite fields GF(2m) using the modified Montgomery modular multiplication (MMM) is presented. The least significant bit (LSB)-first multiplication and two-level parallel computing scheme are considered to improve the cell delay, latency, and area-time (AT) complexity. The proposed method has the features of regularity, modularity, and unidirectional data flow and offers a considerable improvement in AT complexity compared with related multipliers. The proposed multiplier can be used as a kernel circuit for exponentiation/division and multiplication.

Investigation of Small Current Interruption Performance for New Type of Interrupting Chamber in SF$_{6}$ Gas Circuit Breaker (신차단방식 SF$_{6}$ 가스 차단기의 소전류 차단성능 연구)

  • Song, Won-Pyo;Kweon, Ki-Yeoung;Lee, Jae-Sung;Song, Ki-Dong;Kim, Maeng-Hyun;Ko, Hee-Seok
    • The Transactions of the Korean Institute of Electrical Engineers B
    • /
    • v.54 no.11
    • /
    • pp.519-526
    • /
    • 2005
  • This paper presents computer simulation results for developing new type of SF$_{6}$ Circuit Breaker in terms of cold gas flow after small current interruption. This cold gas flows down a nozzle into the chamber of a circuit breaker. There are many difficult problems in analyzing the gas flow due to complex geometry, moving boundary, shock wave and so on. When predicting the dielectric capability of a gas circuit breaker after interruption, the gas pressure and density distributions due to the cold gas must be considered in addition to the electrical field imposed across the gas. A self-coded computational fluid dynamics (CFD) program is used for the simulation of cold gas flow in order to evaluate the electrical field characteristic across open contacts and transient characteristics of insulations after small current interruption.

The Study of Turbulence Model of Low-Reynolds Number Flow (저 레이놀즈수 유동장에서의 난류모델에 관한 연구)

  • Yoo C.;Lee J. S.;Kim C.;Rho O. H.
    • 한국전산유체공학회:학술대회논문집
    • /
    • 2004.03a
    • /
    • pp.172-177
    • /
    • 2004
  • In the present work, we have interests on the modification of parallel implemented with MPI(Message Passing Interface) programming method, 3-Dimensional, unsteady, incompressible Navier-Stokes equation solver to analyze the low-Reynolds number flow In order to accurate calculation aerodynamic coefficients in low-Reynolds number flow field, we modified the two-equation turbulence model. This paper describes the development and validation of a new two-equation model for the prediction of flow transition. It is based on Mentor's low Reynolds $\kappa-\omega$ model with modifications to include Total Stresses Limitation (TSL) and Separation Transition Trigger (STT)

  • PDF

Numerical calculations of aerodynamic performance for ATM train at crosswind conditions

  • Rezvani, Mohammad Ali;Mohebbi, Masoud
    • Wind and Structures
    • /
    • v.18 no.5
    • /
    • pp.529-548
    • /
    • 2014
  • This article presents the unsteady aerodynamic performance of crosswind stability obtained numerically for the ATM train. Results of numerical investigations of airflow past a train under different yawing conditions are summarized. Variations of occurrence flow angle from parallel to normal with respect to the direction of forward train motion resulted in the development of different flow patterns. The numerical simulation addresses the ability to resolve the flow field around the train subjected to relatively large yaw angles with three-dimensional Reynolds-averaged Navier-Stokes equations (RANS). ${\kappa}-{\varepsilon}$ turbulence model solved on a multi-block structured grid using a finite volume method. The massively separated flow for the higher yaw angles on the leeward side of the train justifies the use of RANS, where the results show good agreement with verification results. A method of solution is presented that can predict all aerodynamic coefficients and the wind characteristic curve at variety of angles at different speed.