• 제목/요약/키워드: compute simulation

검색결과 470건 처리시간 0.024초

축방향 난류경계층에서 벽면마찰 섭동량의 공간 및 시간에 따른 특성 (Space-Time Characteristics of the Wall Shear-Stress Fluctuations in a Low-Reynolds Number Axial Turbulent Boundary Layer)

  • 신동신
    • 설비공학논문집
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    • 제15권11호
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    • pp.895-901
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    • 2003
  • Direct numerical simulation database of an axial turbulent boundary layer is used to compute frequency and wave number spectra of the wall shear-stress fluctuations in a low-Reynolds number axial turbulent boundary layer. One-dimensional and two-dimensional power spectra of flow variables are calculated and compared. At low wave numbers and frequencies, the power of streamwise shear stress is larger than that of spanwise shear stress, while the powers of both stresses are almost the same at high wave numbers and frequencies. The frequency/streamwise wave number spectra of the wall flow variables show that large-scale fluctuations to the ms value is largest for the streamwise shear stress, while that of small-scale fluctuations to the rms value is largest for pressure. In the two-point auto-correlations, negative correlation occurs in streamwise separations for pressure and spanwise shear stress, and in spanwise correlation for both shear stresses.

전산유체역학을 통한 PAV의 로터 블레이드 축간거리에 따른 호버링 성능 변화 연구 (A Study on Hovering Performance of Personal Air Vehicle According to Distance between Rotor Blade Axis via Computational Fluid Dynamics)

  • 윤재현;노우승;도재혁
    • 한국기계가공학회지
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    • 제21권5호
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    • pp.53-60
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    • 2022
  • In this study, the conceptual design and performance evaluation of a personal air vehicle (PAV) is presented, which is a potential futuristic individual transportation. The blade element theory (BET) is employed to compute a rotational velocity. A computational fluid dynamics (CFD) simulation is performed to investigate the difference in the thrust performance in the rotor axis distance of a quad-copter PAV in hovering. Modal analysis is performed to create a Campbell diagram to investigate critical speed. Consequently, a quad-copter PAV changes the aerodynamics thrust and critical velocity according to the rotor axis distance.

Sample size calculations for clustered count data based on zero-inflated discrete Weibull regression models

  • Hanna Yoo
    • Communications for Statistical Applications and Methods
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    • 제31권1호
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    • pp.55-64
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    • 2024
  • In this study, we consider the sample size determination problem for clustered count data with many zeros. In general, zero-inflated Poisson and binomial models are commonly used for zero-inflated data; however, in real data the assumptions that should be satisfied when using each model might be violated. We calculate the required sample size based on a discrete Weibull regression model that can handle both underdispersed and overdispersed data types. We use the Monte Carlo simulation to compute the required sample size. With our proposed method, a unified model with a low failure risk can be used to cope with the dispersed data type and handle data with many zeros, which appear in groups or clusters sharing a common variation source. A simulation study shows that our proposed method provides accurate results, revealing that the sample size is affected by the distribution skewness, covariance structure of covariates, and amount of zeros. We apply our method to the pancreas disorder length of the stay data collected from Western Australia.

분지관 내 물체 주위 맥동류에 대한 CFD 해석 (CFD ANALYSIS FOR A PULSATILE FLOW AROUND A BODY INSIDE A BIFURCATED TUBE)

  • 황도연;유성수;이명수;한병윤;박형구
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2009년 춘계학술대회논문집
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    • pp.183-190
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    • 2009
  • The objective of this study is to get simulation data about pulsatile flow around an interior solid body inside a bifurcated tube. All the processes were based on CFD method, with a commercial FVM code, SC/Tetra ver. 6.0 for solving, and with CATIA R16 for generating geometries. The bifurcated tube models were drawn with the bifurcated angle of 45 degrees, considering Murray's law about the diameter ratio. With various locations of the object, the effects of flow on the drag were considered. For the pulsating flow condition, the velocity wave profile was given as the inlet boundary condition. To validate all the result, the simulation was compared with the existing data of the other papers first. Overall flow field of both data were similar, but there was some difference at a zero velocity. Therefore the next simulation was continued with the sine wave profiles where there is no negative flow, and then the data was compared with one of the pulmonary artery velocity where there is negative flow. The final process was to calculate flow variables such as the wall shear stress (WSS) and to compute the drag of the solid object.

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Comparison of steady and unsteady simulation methodologies for predicting no-load speed in Francis turbines

  • Hosseinimanesh, Hossein;Devals, Christophe;Nennemann, Bernd;Guibault, Francois
    • International Journal of Fluid Machinery and Systems
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    • 제8권3호
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    • pp.155-168
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    • 2015
  • No-load speed is an important performance factor for the safe operation of hydropower systems. In turbine design, the manufacturers must conduct several model tests to calculate the accurate value of no-load speed for the complete range of operating conditions, which are expensive and time-consuming. The present study presents steady and unsteady methods for calculating no-load speed of a Francis turbine. The steady simulations are implemented using a commercial flow solver and an iterative algorithm that relies on a smooth relation between turbine torque and speed factor. The unsteady method uses unsteady RANS simulations that have been integrated with a user subroutine to compute and return the value of runner speed, time step and friction torque. The main goal of this research is to evaluate and compare the two methods by calculating turbine dynamic parameters for three test cases consisting of high and medium head Francis turbines. Overall, the numerical results agreed well with experimental data. The unsteady method provided more accurate results in the opening angle range from 20 to 26 degrees. Nevertheless, the steady results showed more consistency than unsteady results for the three different test cases at different operating conditions.

공력면 전개 모사를 위한 공력 모델링 연구 (A Study of Aerodynamic Modelling for Fin Unfolding Motion Analysis)

  • 정석영;윤성준
    • 한국항공우주학회지
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    • 제36권5호
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    • pp.420-427
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    • 2008
  • 접힌 공력면이 전개하는 운동을 모사하기 위하여 전개 운동 방정식을 수립하고 공력면에 작용하는 모멘트 등을 모델링하였다. 공력에 의한 롤 모멘트는 정적 롤 모멘트와 감쇠 모멘트로 이루어져 있으며 정적 롤 모멘트는 전개 하중 측정을 위한 풍동 시험을 통하여 획득한 정적 롤 모멘트 계수로부터 계산된다. 롤 감쇠 계수는 패널법을 이용한 수치 해석을 통하여 산출되었는데 전개 각속도로부터 유발된 받음각에 상응하는 변위각을 공력면에 적용하여 수치해석을 하였다. 공력면 형상에 적용한 변위각은 회전 중심으로부터 공력면 끝단까지 선형적으로 증가하며 회전 중심에서는 변위가 없다. 롤 감쇠 계수는 전개 각속도에 따른 롤 모멘트 계수의 변화율로 계산되며 공력조건과 전개각의 함수이고 전개 각속도에 대해서는 일정하다고 가정하였다. 롤 감쇠를 포함하여 모사된 공력면의 전개 모사는 시험과 비교하여 유사한 결과를 보여주었다.

DSMC 방법을 사용한 KM 잔류추력 밀도장 시뮬레이션 (Simulation of KM Plume Density Field by Residual Thrust Using DSMC Method)

  • 최영인;옥호남;홍일희
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2011년도 제37회 추계학술대회논문집
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    • pp.769-771
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    • 2011
  • KSLV-I 2단에 탑재된 위성은 KM과 충돌하지 않도록 오염 및 충돌 회피 기동(CCAM)을 수행하게 된다. 이때 위성이 KM 잔류 추력 Plume의 밀도가 충분히 낮은 영역을 통과해야만 오염을 피할 수 있으며, 이를 확인하기 위해서는 Plume 유동장의 정확한 예측이 필수적이다. 본 논문에서는 다양한 희박기체 유동해석에 사용되어 그 정확도가 검증된 DSMC 기법을 사용하는 러시아 ITMA 연구소의 SMILE Code를 이용하여 위성과 분리된 KM의 잔류추력에 의한 Plume의 밀도장을 시뮬레이션 하여 분포를 예측하였고, 그 결과의 신뢰성을 확인하기 위하여 KM 노즐 내부의 밀도장은 Fluent의 결과와 비교하여 그 타당성을 입증하였다.

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레이와 텍스처 기법을 이용한 실시간 스프레이 페인팅 (Real-time Spray Painting using Rays and Texture Map)

  • 김대석;박진아
    • 한국정보과학회논문지:컴퓨팅의 실제 및 레터
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    • 제14권8호
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    • pp.818-822
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    • 2008
  • 본 논문에서는 가상환경에서 페인트를 분사하여 시간으로 물체를 도색 하는 시뮬레이션을 위한 충돌처리 및 시각화 알고리즘을 제시한다. 이를 통하여 물체에 페인트가 뿌려지면서 도색 되는 모습을 사실적으로 표현해 줄뿐만 아니라, 페인트 누적 모델을 이용하여 물체에 누적된 페인트의 두께 정보까지 시뮬레이션 하여 시각화함으로써 가상훈련 시스템에 적용할 수 있도록 한다. 분사되는 유체시뮬레이션을 위해서 기존에는 파티클 시스템이 이용되고 있으나 실시간으로 도색이 되는 과정을 시각화하기 위해서는 수백만 개의 파티클에 대하여 충돌 검사를 수행해야 하기 때문에 적절하지 않다. 따라서 본 연구에서는 소수의 레이와 텍스처 기법을 이용하여 효율적으로 충돌 검사를 수행하는 알고리즘을 제안하고 이를 구현하였으며 실시간 페인트 시뮬레이션 구현 결과와 수행 시간 분석을 통하여 알고리즘의 효율성을 검증하였다.

Molecular-dynamic simulation on the equilibrium and dynamical properties of fluids in a nano-channel

  • Hoang, H.;Kang, S.;Suh, Y.K.
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년도 학술대회
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    • pp.208-214
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    • 2008
  • The equilibrium molecular-dynamic simulations have been performed to estimate the properties of the three kinds of fluids (the Lennard-Jones fluid, water and aqueous sodium-chloride solution) confined between two plates that are separated by 1.086 nm; included in the equilibrium properties are the density distribution and the static structure, and the diffusivity in the dynamic property. Three kinds of fluids considered in this study are. The water molecules are modeled by using the SPC/E model and the ions by the charged Lennard-Jones particle model. To treat the water molecules, we combined the quaternion coordinates with Euler angles. We also proposed a plausible algorithm to assign the initial position and direction of molecules. The influence of polarization of water molecules as well as the presence of ions in the solution on the properties will be addressed in this study. In addition, we performed the non-equilibrium molecular-dynamic simulation to compute the flow velocity for the case with the gravitational force acting on molecules.

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Molecular-dynamic simulation on the equilibrium and dynamical properties of fluids in a nano-channel

  • Hoang, H.;Kang, S.;Suh, Y.K.
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년 추계학술대회논문집
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    • pp.208-214
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    • 2008
  • The equilibrium molecular-dynamic simulations have been performed to estimate the properties of the three kinds of fluids (the Lennard-Jones fluid, water and aqueous sodium-chloride solution) confined between two plates that are separated by 1.086 nm; included in the equilibrium properties are the density distribution and the static structure, and the diffusivity in the dynamic property. Three kinds of fluids considered in this study are. The water molecules are modeled by using the SPC/E model and the ions by the charged Lennard-Jones particle model. To treat the water molecules, we combined the quaternion coordinates with Euler angles. We also proposed a plausible algorithm to assign the initial position and direction of molecules. The influence of polarization of water molecules as well as the presence of ions in the solution on the properties will be addressed in this study. In addition, we performed the non-equilibrium molecular-dynamic simulation to compute the flow velocity for the case with the gravitational force acting on molecules.

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