• 제목/요약/키워드: 수치유체해석

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Analysis of Motion of Batoid Fins for Thrust Generation by Using Fluid-Structure Interaction Method (추진력 생성을 위한 가오리 날개 짓의 유체-구조연성 수치해석)

  • Kwon, Dong-Hyun;Lee, Jong-Soo
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.34 no.11
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    • pp.1575-1580
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    • 2010
  • Recently, the development of bio-mimetic underwater vehicles that can emulate the characteristic movements of marine fish and mammals has attracted considerable attention. In this study, the motion of the batoid (i.e., cownose ray) fin that facilitates excellent cruising and maneuvering during underwater movement has been studied. The velocity achieved and distance covered with each fin movement are numerically studied. A fluid-structure interaction method is used to perform 3D time-dependent numerical analysis, wherein an adaptive mesh is employed to account for the large deformation of a fin interacting with a fluid. The results of a preliminary study show that the thrust of a ray fin is highly dependent on the frequency. Further, once the fin amplitude required for generating a given thrust is evaluated for the conditions experienced by an actual ray, the frequency and amplitude values for achieving better thrust are determined.

Interaction Analysis between Waves and Caissons by Damping Zone Effect for Installing New Caisson on Old Caisson Breakwater (기존 케이슨방파제에 신규 케이슨 추가설치 시 댐핑존 영향에 따른 유체와 케이슨들간의 상호작용 평가)

  • Park, Min Su;Kim, Young Taek;Park, Sangki;Min, Jiyoung
    • Journal of Korean Society of Coastal and Ocean Engineers
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    • v.34 no.5
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    • pp.156-168
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    • 2022
  • The design and construction are carried out to improve the structural stability of caisson breakwaters by installing new caissons on the front or rear of old caissons. The wave forces acting on caisson are excessively calculated by the resonance of fluid existing between the old caisson and the new caisson in the numerical analysis using potential flow. In this study, we used the damping zone option in ANSYS AQWA program to analyze the wave forces acting on individual caissons according to the interaction effects between the incident wave and the caisson. By applying the damping zone option to the fluid in which resonance occurs, the wave forces acting on individual caissons were calculated by the change of damping factor. In addition, the wave force characteristics acting on individual caissons were analyzed for the different distances between caissons in the frequency domain analysis.

River Hydraulic Analysis and Application Using EFDC Model Focused on Geumgang Weir Section (EFDC 모형을 이용한 금강보 구간 하천수리해석 및 적용성 검토)

  • Seo, Sung-Ho;Hur, Young-Teck;Jeong, Sang-Man
    • Proceedings of the Korea Water Resources Association Conference
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    • 2011.05a
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    • pp.39-39
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    • 2011
  • 하천에서 수공구조물을 설계시 구조물의 규모, 형식, 운영방식, 안정성 등을 검토하기 위하여 일반적으로 수리모형실험과 수치모형실험을 이용한다. 수리모형실험은 자연현상의 왜곡을 최소화하여 검토결과를 얻을 수 있다는 장점이 있지만, 많은 시간과 비용, 인력 및 공간이 필요하기 때문에 단기간에 다양한 검토가 필요한 경우에는 많은 제약이 따른다. 반면에 수치모형실험은 제한적인 조건에서 검토목적 및 용도에 따라 다양한 수치모의기법을 활용하여 상대적으로 낮은 비용과 신속하고 다양한 검토가 가능하다는 장점을 가지고 있다. 그러나 수치모형실험은 어디까지나 자연현상에 대한 수학적, 물리적 기법을 활용한 분석이기 때문에 결과에 대한 신뢰성 확보가 매우 중요하다. 최근에는 컴퓨터의 계산능력 향상과 유체의 복잡한 동수역학적 거동 해석 기법의 다양화, 그리고 많은 적용성 검토 연구결과로 인한 신뢰성 향상 등으로 인해 수치모형실험에 대한 관심이 높아지고 있다. 본 연구는 현재 금강에 건설 중인 금강보에 대하여 다차원 수치모형인 EFDC(Environmental Fluid Dynamics Code)를 이용하여 하천 구조물 및 물리적 환경변화에 대한 정밀수리분석을 실시하기 위한 사전절차로, EFDC 모형을 하천수리해석에 적용할 경우 모형에 포함되어 있는 다양한 변수설정 및 제약조건들에 대하여 적용한계를 검토하고자 한다. 검토방법은 금강보가 건설되기 이전의 하천지형 상황에서 EFDC 모형과 HEC-RAS 모형을 이용한 수리분석을 수행하고, 수리거동 결과 들을 상호 비교 분석 한다. 수치모의 대상구간은 금강보 건설구간을 포함하여 약 20km 구간이고, 대상구간에 대하여 3차원 정밀지형자료를 구축하였으며, 과거 호우사상에 대한 구간 내 관측 수위 및 모형별 계산수위결과를 비교 검토하였다.

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Dynamic Characteristics Simulation for a Simplex Swirl Injector (스월 인젝터의 동특성에 대한 수치해석 연구)

  • 박홍복
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.34 no.9
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    • pp.67-75
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    • 2006
  • A fully nonlinear model accounting for swirling effect has been applied in analyzing the dynamic response for a classical swirl injector. The current work applied highly accurate Boundary Element Methods (BEMs) in assessing its static and dynamic characteristics. On the basis of moving surface treatment method and surface instability study, which are obtained from the previous static characteristics analysis in pressure-swirl injectors, this work was expanded for analyzing the dynamics of a classical swirl injector. The dynamic response through injector components for disturbed inflow condition was investigated. The modified code was validated from comparison with the theoretical result for a typical swirl injector. Clearly the simulated result shows the interesting characteristics of swirl injectors to provide either amplification or damping of the input disturbance through each component. These results give promise in applying the current model to nonlinear dynamic characteristics of swirl injectors.

Dynamic Response Analysis of Pipe Subjected to Underwater Explosion (수중폭발로 인한 파이프의 동적 응답해석)

  • Kim, Seongbeom;Lee, Kyungjae;Jung, Dongho;Park, Taehyo
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.34 no.1
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    • pp.9-16
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    • 2014
  • In recent years, the structural shock response to UNDEX (UNDerwater EXplosion) has been studied as much, or more, through numerical simulations than through testing for several reasons. Very high costs and sensitive environmental concerns have kept destructive underwater explosion testing to a minimum. Increase of simulation capabilities and sophisticated simulation tools has made numerical simulations more efficient analysis methods as well as more reliable testing aids. In this study, the main issue is the fluid-structure interaction. Here, appropriate relations between the acoustic pressure on the fluid surface and displacements on the structure surface are formed internally. The analysis was carried out using ABAQUS/Explicit and the results have been visualized in ABAQUS CAE. The shock loading history, acoustic pressure, stress of stand-off point, the velocity and strain energy time histories were presented.

Numerical Analysis of Hydrodynamic Forces on a Floating Body in Two-layer Fluids (밀도가 상이한 두 유체층에서 부유체 동유체력 특성의 수치적 해석)

  • Kim, Mi-Geun;Koo, Weon-Cheol
    • Journal of the Society of Naval Architects of Korea
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    • v.47 no.3
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    • pp.369-376
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    • 2010
  • In this study, a radiation and a diffraction problems of a floating body in two-layer fluids were solved by the Numerical Wave Tank(NWT) technique in the frequency domain. In two-layer fluids, two different wave modes exist and the hydrodynamic coefficients can be obtained separately for each mode. The two-domain Boundary Element Method(BEM) in the potential fluid using the whole-domain matrix scheme was used to investigate the characteristics of wave forces, added mass and damping coefficients. The effects of the ratio of density and water depth in the lower domain were also evaluated and compared with given references.

MQUICK Upwind Scheme for the Incompressible Navier-Stokes Equations (비압축성 Navier-Stokes 방정식의 해석을 위한 MQUICK 상류해법)

  • Shin B. R.;Ikohagi T.
    • Journal of computational fluids engineering
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    • v.4 no.1
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    • pp.41-52
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    • 1999
  • 이 논문에서는, QUICK해법의 불안정성을 개량하므로써, 수치계산에 있어서 수렴이 빠르고, 수치적으로 안정한 계산을 할 수 있는 새로운 MQUICK 상류해법을 제안하고, 이를 비압축성 층류유동의 계산에 적용하였다. 또한, 해법의 정확성, 안정성, 수렴속도에 대한 검토를 통하여 본 MQUICK 상류해법의 유효성과 타당성이 평가되었다. 이 해법에서는 인공산일의 가감을 조절하기 위하여 가중계수 α를 써서 정식화 하였고, 위의 검토를 통하여 α의 최적값을 조사하였다. 이 해법을 SMAC 음해법에 적용하여 2 차원 공동유동, 3 차원 덕트유동과 같은 몇몇 표준문제를 계산하고, 계산된 결과를 실험값 또는, 3 차 정확도의 상류해법 및 QUICK해법에 의한 결과 들과 비교 하므로써, 본 MQUICK 상류해법이 위의 다른 해법에 비하여 안정하고, 유효성이 높은 해법임을 확인 하였다.

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Study on Measurement and Numerical Analysis for Fluid Flow past a Circular Cylinder in Rectangular Duct (사각던트 내에서 원형 실린더를 지나는 유체유동의 측정 및 수치해석에 관한 연구)

  • 김경환;윤영환
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.15 no.12
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    • pp.1095-1102
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    • 2003
  • Flow characteristics of turbulent steady fluid flow past a cylinder in rectangular duct are measured by 5 W laser doppler velocity meter. The fluid flow is also computed by commercial software of STAR-CD for comparison between the measurement and computation. The turbulent models applied in the computations are standard K-epsilon model, RNG K-epsilon model and Chen K-epsilon model. Acurracy of standard K-epsilon model is a little bit better than acurracies of other models even though those models have almost the same order of error compared to measured data. The computations predict satisfactorily the measured velocity profiles at middle section of the circular cylinder before the fluid flow diverges. However, there are some disagreements between them at down stream from the circular cylinder.

Hybrid RANS/LES Simulation of Subsonic Cavity Flow (Hybrid RANS/LES 방법을 이용한 이음속 공동 유동의 수치적 모사)

  • Chang K. S.;Park S. O.;Choi S. K.
    • Journal of computational fluids engineering
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    • v.9 no.2
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    • pp.23-29
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    • 2004
  • A numerical simulation of an incompressible cavity flow is conducted using the hybrid turbulence model. The model adopted is a modified type of DES using k- ε two-equation model. Cavity geometry and flow condition are based on Cattafesta's experiment. Computational results are compared with the results of Cattafesta's experiment. The simulation successfully predicts the oscillatory features and the Strouhal number of the oscillation compares very favorably with that of the dominant mode of experimental data. Vorticity contours obtained from the simulation data are consistent with the smoke visualization of the Cattafesta's experiment. The coherent structures of cavity flow are also investigated using Q criterion.

EFFICIENT SIMULATION AND SCALING OF OSCILLATORY IMPINGING JETS (진동하는 충돌 제트의 스케일링과 효율적인 수치 모사)

  • Kim S. I.;Park S. O.;Hong S. K.;Lee K. S.
    • Journal of computational fluids engineering
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    • v.10 no.4 s.31
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    • pp.32-38
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    • 2005
  • Present study simulates oscillatory supersonic impinging jet flows using the axisymmetric Navier-Stokes code. To capture the salient features of flow oscillation and overcome the divergence during the initial transient period, several tests have been conducted for the grid and time step sizes. The results also show that the effects of the inlet flow condition at the nozzle exit and turbulence on the oscillatory behavior of supersonic impinging jets are negligible. Frequencies of the surface pressure oscillation obtained by the selected numerical method are in good accord with the measured impinging tones for various cases of nozzle-to-plate distance. Two seemingly different staging behaviors with nozzle-to-plate distance and nozzle pressure variations are found to correlate well if the frequency and distance are normalized by the length of the first shock cell.