• Title/Summary/Keyword: 3차원 정상유동

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Development of Steady/Unsteady Aerodynamic Analysis Program Using 3-Dimensional Subsonic Unstructured Panel Method (3차원 아음속 비정렬 패널법을 이용한 정상/비정상 공력 해석 프로그램 개발)

  • Park, Jinyi;Baek, Chung;Lee, Seungsoo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.50 no.6
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    • pp.367-376
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    • 2022
  • In this study, a steady and unsteady aerodynamic analysis program using a 3-dimensional subsonic unstructured panel method is developed and verified. Surfaces of bodies are modeled with the source and doublet distributions on triangular or quadrilateral panels. Geometry modeling of complex geometries and multi-body, therefore, can be easily accomplished. The Kelvin theory and the unsteady Kutta condition allow the doublet strength of the wake panels determined for unsteady flows. Various steady and unsteady flows in two and three dimensions are computed and compared with the analytical and the published computational results.

Flow Dimensional Analysis for Constant Pressure Injection Test (정압주입시험을 이용한 지하수유동차원 해석)

  • 이은용
    • The Journal of Engineering Geology
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    • v.3 no.2
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    • pp.149-165
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    • 1993
  • Nowadays, the field hydraulic test is still an only method to evaluate groundwater characteristics in subsurface. The results of hydraulic test are very important for the concept model of fracture hydrogeology as well as the geometric pattern of fractures. The hydraulic tests performed in Korea are generally analysed under such assumption as steady radial flow in homogeneous aquifer or along simple geometry of fractures. Also the transmissivity measured in a fixed interval length is equivalent to a sum of individual fracture transmissivities in test legth. The boundary effects of weH hydraulics and the geometry of flow paths are hardly obtained from the test results analysed by a steady flow method. To circumvent this problem, the flow dimensional analysis was attempted from the results of constant pressure injection test carried out in a fractured granite area. A comparison of the hydraulic conductivity values from the transient and steady analysis shows that the latter is about a factor of 2~3 higher than the former. However, it was possible to analyse a flow dimension of each test interval from flow rate variation with time. The upper part of the bedrock(<10m deep) indicates an open boundary and the flow dimension shows nearly steady states, while the lower part of the bedrock(>25m deep) is characterized as sublinear flow dimension with a dosed boundary. In one of the test sections(15m deep), the flow dimension was changed from linear flow to spherical flow. From the experience of this study, one of the immediate problems to be solved is to enhance the field testing equipments, i.e., an accurate flowmeter with autorecording and a pressure detecting device to be able to install in the test section.

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Experimental Study on the Aerodynamic Characteristics of the Ducted fan for the Propulsion of a Small UAV (소형 무인항공기 추진용 덕티드팬의 공력특성에 대한 실험적 연구)

  • Ryu, Min-Hyoung;Cho, Lee-Sang;Cho, Jin-Soo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.40 no.5
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    • pp.413-422
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    • 2012
  • The ducted fan for a small UAV propulsion can reconnoiter and observe in a town and a small area, it has better thrust efficiency and a long endurance than propeller. Thrust characteristics of hover and for ward flight condition for the ducted fan UAV is important issue to improve a endurance. The unsteady 3-dimensional flow fields of the ducted fan UAV is essential to stable flight. In this paper, to verify the design results of the ducted fan and to investigate a stable aeronautical characteristic, the thrust performance and the unsteady 3-dimensional flow fields are measured. Thrust characteristics for the hovering and the forward flight conditions are measured by the 6-components balance system in the subsonic wind tunnel. The unsteady 3-dimensional flow fields are analyzed by using a stationary $45^{\circ}$ slanted hot-wire technique. The swirl velocity is almost removed behind the stator blades. Therefore, the thrust performance of the ducted fan is improved and the flight stability is maintained.

Groundwater Flow Analysis Using a Transient Three-dimensional Model in an Upland Area (삼차원(三次元) 비정상(非定常) 지하수모형(地下水模型)에 의한 홍적대지의 지하수(地下水) 유동해석(流動解析))

  • Bae, Sang Keun
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.10 no.2
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    • pp.59-65
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    • 1990
  • This study investigates the effects of human impact and precipitation on groundwater flow conditions at a small area in Dejima Upland using a transient three-dimensional simulation. To show the utility of the transient three-dimensional model, the results of the numerical model are compared with those of Theis problem for which analytical solution is available. It appears that over the time period studied, the results of the model agree well with the analytical solution. Simulation is undertaken for a period of 30days starting from May 1st, when irrigation starts. Groundwater flow patterns determined by a numerical model are presented in the form of plotted potential lines and discussed. Results of simulation clearly indicate that the groundwater flow system should be analysed using a transient three-dimensional model, especially for the region which is effected by human impact.

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Experimental Study on the Unsteady Flow Characteristics of the Counter-Rotating Axial Flow Fan (엇회전식 축류팬의 비정상 유동특성에 관한 실험적 연구)

  • Cho, Lee-Sang;Choi, Hyun-Min;Kang, Jeong-Seek;Cho, Jin-Soo
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2007.11a
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    • pp.305-310
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    • 2007
  • For the understanding of the complex flow characteristics in the counter-rotating axial flow fan, it is necessary to investigate the three-dimensional unsteady flow fields in the counter-rotating axial flow fan. This information is also essential for the prediction of the aerodynamic and acoustical characteristics of the counter-rotating axial flow fan. Experimental study on the three-dimensional unsteady flow in the counter-rotating axial flow fan is carried out at the design point(operating condition). Three-dimensional unsteady flow fields in the counter rotating axial flow fan are measured at the cross-sectional planes of the upstream and downstream of each rotor using the $45^{\circ}$ inclined hot-wire. Three-dimensional unsteady flow fields in the counter-rotating axial flow such as the wake, the tip vortex and the tip leakage flow are shown the form of the velocity vectors and the velocity contours.

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Comparative Evaluation of Three-dimensional Turbulence Models in Coastal Region (연안 해수유동에 관한 3차원 난류모형의 비교평가)

  • 정태성
    • Journal of Korean Society of Coastal and Ocean Engineers
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    • v.8 no.3
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    • pp.256-267
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    • 1996
  • In estuarine 3-dimensional numerical modeling. it is very important to calculate vertical eddy viscosity accurately. Various turbulence models employing eddy viscosity concept were applied to the steady flow in an open-channel and the tidal flow in long tidal channel and compared. The evaluations include the verification tests against experimental data sets for steady and tidal flows. The simulation results have shown that the compared models are in good agreements with experimental data of steady flow while only $textsc{k}$-$\varepsilon$ model, $textsc{k}$-ι model, and 1-equation model with well-defined mixing length profile give good agreements with experimental data of tidal flow.

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Numerical Study on Steady and Unsteady Flow Characteristics of Nozzle-Rotor Flow in a Partial Admission Supersonic Axial Turbine with Sweep Angle (스윕 각이 적용된 부분 흡입형 초음속 축류 터빈의 정상, 비정상 공력 특성에 관한 수치적 연구)

  • Jeong, Soo-In;Kim, Kui-Soon
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2012.05a
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    • pp.173-179
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    • 2012
  • Steady and unsteady three-dimensional RANS simulations have been performed on partial admission supersonic axial turbine having backward/forward sweep angles(${\pm}15^{\circ}$) and the results are compared with each other. The objective of this paper is to study the effect of unsteadiness on turbine flow characteristics and performances. The all results indicated that the losses of unsteady simulations were greater than those of steady cases. It was also shown that BSW model give the effect on the reducing of mass flow rates of tip leakage. In unsteady simulation, the increase of t-to-s efficiency at Rotor Out plane was observed more clearly.

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Unsteady Three-Dimensional Analysis of Transverse Fuel Injection into a Supersonic Crossflow using Detached Eddy Simulation Part II : Reacting Flowfield (DES를 이용한 초음속 유동내 수직 연료분사 유동의 비정상 3차원 해석 Part II : 반응 유동장)

  • Won, Su-Hee;Jeung, In-Seuck;Choi, Jeong-Yeol
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.37 no.9
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    • pp.879-888
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    • 2009
  • Unsteady three-dimensional reacting flowfield generated by transverse hydrogen injection into a supersonic mainstream is numerically investigated using DES and finite-rate chemistry model. Comparisons are made with experimental results to investigate the turbulent reacting flow physics. The numerical OH distribution describes well the experimental OH-PLIF result, while the numerical ignition delay time shows some disparity due to the restricted available experimental data. The intermittency phenomena are identified by the comparative analysis between RANS and DES. Those effects are also quantified by the temperature distributions along streamlines and superimposed OH mass fraction along with time.

A Particle Tracking Method for the Lagrangian-Eulerian Finite Element Method in 3-D Subsurface System (3차원 지표하 시스템에서 Lagrangian-Eulerian 유한요소법에 대한 입자추적 알고리즘)

  • Lee, Jae-Young;Kang, Mee-A
    • The Journal of Engineering Geology
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    • v.19 no.2
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    • pp.205-215
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    • 2009
  • The conventional numerical models to analyze flow in subsurface porous media under the transient state usually generate numerical oscillation and unstability due to local flux domain for critical cases such as infiltration into initially dry soil during rainfall period. In this case, it is required refined mesh and small time step, but it decrease efficiency of computation. In this study, numerical unstability in discontinuity domain is removed by applying particle tracking algorithm to simulate unsteady subsurface flow with inflow boundary condition. Finally the hybrid LE FEM improving numerical stability is proposed. The hypothetical domains with unsteady uniform and nonuniform flow field were used to demonstrated algorithm verification. In comparison with analytic solution, we obtained reasonable results and conducted simulation of hypothetical 3-D recharge/pumping area. The proposed algorithm can simulate saturated/unsaturated porous media with more practical problems and will greatly contribute to accuracy and stability of numerical computation.

Calculation of three-dimensional flow in turbo impellers (터어보 回轉車 內의 3次元 流動의 數値計算)

  • 조강래;방영석
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.10 no.5
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    • pp.751-757
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    • 1986
  • A three-dimensional calculation is presented on the basis of Wu's theory of quasi-three-dimensional flow in turbo impellers. For the calculation of flow on the Blade-to-Blade stream surface, the finite element method is applied. In this work it is shown that the Kutta condition and the periodicity can be satisfied rationally by the technique of combining a basic through flow in the flow passage and a circulating flow around the blade. The results of numerical calculation are compared with those of the exact solution of the Gostelow's straight cascade and of the experimental results of pressure distribution on the rotating blade surface. It is found that the numerical solutions are in good agreement with the theoretical solution and the experimental results.