• 제목/요약/키워드: coupled stokes equations

검색결과 141건 처리시간 0.028초

열파퍼식 가스차단기에서 발생하는 아크 플라즈마에 의한 열유동 특성 (Thermal Flow Characteristics Driven by Arc Plasmas in a Thermal Puffer Type GCB)

  • 이종철;김윤제
    • 대한전기학회논문지:전기기기및에너지변환시스템부문B
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    • 제54권11호
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    • pp.527-532
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    • 2005
  • During the last ten years the new interruption techniques, which use the arc energy itself to increase the pressure inside a chamber by the PTFE nozzle ablation, have displaced the puffer circuit breakers due to reduced driving forces and better maintainability. In this paper, we have investigated the thermal flow characteristics inside a thermal puffer type gas circuit breaker by solving the Wavier-Stokes equations coupled with Maxwell's equations for considering all instabilities effects such as turbulence and Lorentz forces by transient arc plasmas. These relative inexpensive computer simulations might help the engineer research and design the new interrupter in order to downscale and uprating the GIS integral.

A Thermo chemical Study of Arcjet Thruster Flow Field

  • J-R. Shin;S. Oh;Park, J-Y
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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    • pp.257-261
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    • 2004
  • Computational fluid dynamics analysis was carried out for thermo-chemical flow field in Arcjet thruster with mono-propellant Hydrazine ($N_2$H$_4$) as a working fluid. The theoretical formulation is based on the Reynolds Averaged Navier-Stokes equations for compressible flows with thermal radiation. The electric potential field governed by Maxwell equation is loosely coupled with the fluid dynamics equations through the Ohm heating and Lorentz force. Chemical reactions were assumed being infinitely fast due to the high temperature field inside the arcjet thruster. An equilibrium chemistry module for nitrogen-hydrogen mixture and a thermal radiation module for optically thin media were incorporated with the fluid dynamics code. Thermo-physical process inside the arcjet thruster was understood from the flow field results and the performance prediction shows that the thrust force is increased by amount of 3 times with 0.6KW arc heating.

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하이드라진(N2H4) 아크젯 추력기의 수치적 모델링 (Numerical Modeling of Hydrazine-Fueled Arcjet Thruster)

  • 신재렬;이대성;오세종;최정열
    • 한국항공우주학회지
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    • 제36권9호
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    • pp.907-915
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    • 2008
  • 하이드라진(N2H4) 아크젯 추력기의 열화학 유동장 해석을 위한 전산유체해석을 수행하였다. 열복사와 전기장이 고려된 압축성 유동해석을 위해서 RANS 방정식을 수정하여 사용하였다. 로렌츠 힘과 Ohm 가열효과를 고려한 Maxwell 방정식이 유동방정식과 결합되어 전기 방전으로 인한 전기장해석을 위해 이용되었다. 아크젯 추력기 내부에서 유동장은 충분히 고온상태이기에 화학평형 해석이 이용되었으며, 광학 두께를 이용한 열복사 모델이 유동방정식에 적용되었다. 계산 결과들은 아크젯 추력기유동이 동결유동에 비해 추력은 180%증가되며, 비추력은 200%가까이 상승됨을 보여준다. 또한 유동장 해석 결과들은 아크젯 추력기 내부의 열적 물리적 특성에 대한 이해를 돕는다.

고정된 직사각형 격자계에서 움직이는 물체주위 자유수면유동 계산을 위한 수치기법의 개발 (A NUMERICAL SIMULATION METHOD FOR FREE SURFACE FLOWS NEAR MOVING BODIES IN A FIXED RECTANGULAR GRID SYSTEM)

  • 정광열;이영길;하윤진
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2011년 춘계학술대회논문집
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    • pp.395-406
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    • 2011
  • In this research a numerical simulation method is developed for moving body in free surface flows using fixed staggered rectangular grid system. The non-linear free surface near the body is defined by marker-density method. The body boundary is defined by line segment connecting the points where the body surface and grid line meet. Continuity equation and Navier-Stokes equations are used as governing equations and the equations are coupled with two-step projection method. The velocities and pressures of body boundary and free surface cells are calculated with simultaneous iterative method. To treat a body movement in a fixed grid system, the volume displaced by moving body is added to the divergence of the body boundary cell. For the verification of the present numerical method. vortex shedding period of advancing cylinder is calculated and the period is compared with existing experiment results. Moreover, added mass and damping coefficients of a vertically excited box are calculated and the computed results are compared with published experiment results. Impulsive pressure and water level variation due to sloshing phenomenon are simulated and the results are compared with published experiment results. Varying the plunger shape, the waves generated by plunging type wave maker are compared with the 2nd order Stokes wave theory The plunger shape generating the wave that shows the best agreement with the theory is represented.

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Properties of Inductively coupled Ar/CH4 plasma based on plasma diagnostics with fluid simulation

  • 차주홍;손의정;윤용수;한문기;김동현;이호준
    • 한국진공학회:학술대회논문집
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    • 한국진공학회 2016년도 제50회 동계 정기학술대회 초록집
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    • pp.210.2-210.2
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    • 2016
  • An inductively coupled plasma source was prepared for the deposition of a-C:H thin film. Properties of the inductively coupled plasma source are investigated by fluid simulation including Navier-Stokes equations and home-made tuned single Langmuir probe. Signal attenuation ratios of the Langmuir probe harmonic frequency were 13.56Mhz and 27.12Mhz. Dependencies of plasma parameters on process parameters were accord with simulation results. Ar/CH4 plasma simulation results shown that hydrocarbon radical densities have their lowest value at the vicinity of gas feeding line due to high flow velocity. For input power density of 0.07W/cm3, CH radical density qualitatively follows electron density distribution. On the other hand, central region of the chamber become deficient in CH3 radical due to high dissociation rate accompanied with high electron density. The result suggest that optimization of discharge power is important for controlling deposition film quality in high density plasma sources.

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Characterization of inductively coupled Ar/CH4 plasma using tuned single langmuir probe and fluid simulation

  • 차주홍;한문기;김동현;이해준;이호준
    • 한국진공학회:학술대회논문집
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    • 한국진공학회 2015년도 제49회 하계 정기학술대회 초록집
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    • pp.143.1-143.1
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    • 2015
  • An inductively coupled plasma source driven by 13.56MHz was prepared for the deposition of a-C:H thin film. Properties of the plasma source are investigated by fluid simulation including Navier-Stokes equations and home-made tuned single Langmuir probe. Signal attenuation ratios of the Langmuir probe at first and second harmonic frequency were 13.56Mhz and 27.12Mhz respectively. Dependencies of plasma parameters on process parameters were agreed with simulation results. Ar/CH4 plasma simulation results shown that hydrocarbon radical densities have their lowest value at the vicinity of gas feeding line due to high flow velocity. For input power density of 0.07W/cm3, CH radical density qualitatively follows electron density distribution. On the other hand, central region of the chamber become deficient in CH3 radical due to high dissociation rate accompanied with high electron density. The result suggest that optimization of discharge power is important for controlling deposition film quality in high density plasma sources.

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A study on the dynamic instabilities of a smart embedded micro-shell induced by a pulsating flow: A nonlocal piezoelastic approach

  • Atabakhshian, Vahid;Shooshtaria, Alireza
    • Advances in nano research
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    • 제9권3호
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    • pp.133-145
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    • 2020
  • In this study, nonlinear vibrations and dynamic instabilities of a smart embedded micro shell conveying varied fluid flow and subjected to the combined electro-thermo-mechanical loadings are investigated. With the aim of designing new hydraulic sensors and actuators, the piezoelectric materials are employed for the body and the effects of applying electric field on the stability of the system as well as the induced voltage due to the dynamic behavior of the system are studied. The nonlocal piezoelasticity theory and the nonlinear cylindrical shell model in conjunction with the energy approach are utilized to mathematically modeling of the structure. The fluid flow is assumed to be isentropic, incompressible and fully develop, and for more generality of the problem both steady and time dependent flow regimes are considered. The mathematical modeling of fluid flow is also carried out based on a scalar potential function, time mean Navier-Stokes equations and the theory of slip boundary condition. Employing the modified Lagrange equations for open systems, the nonlinear coupled governing equations of motion are achieved and solved via the state space problem; forth order numerical integration and Bolotin's method. In the numerical results, a comprehensive discussion is made on the dynamical instabilities of the system (such as divergence, flutter and parametric resonance). We found that applying positive electric potential field will improve the stability of the system as an actuator or vibration amplitude controller in the micro electro mechanical systems.

하이드라진 아크 추력기의 열화학적 성능해석 (Thermochemical Performance Analysis of Hydrazine Arc Thruster)

  • 신재렬;오세종;최정열
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2005년도 제24회 춘계학술대회논문집
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    • pp.35-38
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    • 2005
  • 하이드라진을 추진제로 쓰는 아크젯 추력기 내의 열화학적 유동장을 전산유체를 이용해 해석하였다. Ohm가열 및 Lorentz힘을 고려하기 위하여 Maxwell 방정식과 연계된 RANS 방정식을 이용하였으며, 매우 빠른 반응 및 광학적으로 두꺼운 매질을 가정하여 하이드라진의 화학 반응과 열복사를 해석에 포함하였다. 아크젯 추력기 내부 유동의 열-물리적 이해와 더불어, 해석의 결과는 0.6 kW의 가열에 의하여 성능지표인 추력과 비추력이 각각 $20\%와 200\%$가 향상됨을 보여준다.

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이온화를 고려한 Arcjet 추력기의 화학 평형 유동 및 성능해석 (Chemical Equilibrium Flow and Performance Analysis of the Arcjet Thruster with Ionization Effects)

  • 신재렬;오세종;최정열
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2005년도 제25회 추계학술대회논문집
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    • pp.132-135
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    • 2005
  • 하이드라진을 추진제로 쓰는 아크젯 추력기 내의 열화학적 유동장을 전산유체를 이용해 해석하였다. Ohm가열 및 Lorentz힘을 고려하기 위하여 Maxwell 방정식과 연계된 RANS 방정식을 이용하였으며, 매우 빠른 반응 및 광학적으로 두꺼운 매질을 가정하여 이온화와 열복사를 해석에 포함하였다. 해석의 결과는 아크젯 추력기 내부 유동의 열-물리적 이해와 더불어 0.6 kW 가열에 의하여 하였을 때 추력과 비추력이 각각 20%와 70%가 향상됨을 보여주었다.

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회전과 유동박리효과를 고려한 3차원 풍력발전 터빈 블레이드의 공탄성 응답 해석 (Aeroelastic Response Analysis of 3D Wind Turbine Blade Considering Rotating and Flow Separation Effects)

  • 김동현;김요한;김동만;김유성;황미현
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2009년도 춘계학술대회 논문집
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    • pp.68-75
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    • 2009
  • In this study, aeroelastic response analyses have been conducted for a 3D wind turbine blade model. Advanced computational analysis system based on computational fluid dynamics(CFD) and computational structural dynamics(CSD) has been developed in order to investigate detailed dynamic responsed of wind turbine blade. Vibration analyses of rotating wind-turbine blade have been conducted using the general nonlinear finite element program, SAMCEF (Ver.6.3). Reynolds-averaged Navier-Stokes (RANS)equations with spalart-allmaras turbulence model are solved for unsteady flow problems of the rotating turbine blade model. A fully implicit time marching scheme based on the Newmark direct integration method is used for computing the coupled aeroelastic governing equations of the 3D turbine blade for fluid-structure interaction (FSI) problems. Detailed dynamic responses and instantaneous Mach contour on the blade surfaces considering flow-separation effects are presented to show the multi-physical phenomenon of the rotating wind-turbine blade model.

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