• 제목/요약/키워드: Rotational flow

검색결과 521건 처리시간 0.022초

스마트 무인기용 터보제트 엔진의 천이성능 모사 (A Transient Performance Simulation of a Smart UAV Turbojet Engine)

  • 공창덕;강명철;기자영;양수석
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2003년도 제21회 추계학술대회 논문집
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    • pp.257-260
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    • 2003
  • 스마트 무인기용 터보제트 엔진의 동적 성능모사 프로그램을 개발하였다. 천이 성능 프로그램에는 일정공기유량(Constant Mass Plow) 방법을 적용되었으며 잉여토크의 적분에는 오일러 적분법을 이용하였다. 천이성능해석은 가스발생기의 아이들로부터 최대 회전수까지 증가하는 것을 수행하였다. 엔진의 동적거동을 살펴보기 연료유량을 step과 ramp 증가로 주었다. 연료가 step으로 증가되었을 때 터빈 입구온도에서 오버슈트가 발생하였으며 연료유량을 0.6sec 이상으로 증가시켰을 때 오버슈트가 제거됨을 확인할 수 있었다.

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사판식 유압 피스톤 펌프의 슬리퍼 정압베어링면 형상에 관한 이론해석 (Theoretical Analysis of the Slipper Hydrostatic Bearing Shape in the Swash Plate Type Axial Piston Pump)

  • 조인성
    • 드라이브 ㆍ 컨트롤
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    • 제10권1호
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    • pp.14-20
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    • 2013
  • In the high rotational speed and pressure state, the leakage flow rate of the axial piston pump is one of the serious problems and make great reasons to decrease the volume efficiency. In this study, tribology characteristics is clarified for the hydrostatic slipper bearing in the swash plate type axial piston pump, by means of theoretical analysis for the different shape of the hydrostatic slipper bearing. It was analyzed by Mathcad software and used equal conditions at $0^{\circ}$ swash plate angle in each model. The results show that performance characteristics of the swash plate type axial piston pump are significantly influenced by the shape of the hydrostatic slipper bearing.

난류 경계층 유동에서 입자의 확산과 스핀의 영향 (Particle Dispersion and Effect of Spin in the Turbulent Boundary Layer Flow)

  • 김병구;이창훈
    • 대한기계학회논문집B
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    • 제28권1호
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    • pp.89-98
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    • 2004
  • In this paper, we develope a dispersion model based on the Generalized Langevin Model. Thomson's well-mixed condition is the well known criterion to determine particle dispersion. But, it has 'non-uniqueness problem'. To resolve this, we adopt a turbulent model which is a new approach in this field of study. Our model was greatly simplified under the self-similarity condition, leaving model only two model constants $C_{0}$ and ${\gamma}$$_{5}$ that control the dispersion and spin which measures rotational property of the Lagrangian particle trajectory. We investigated the sign of spin as well as magnitude by using the Direct Numerical Simulation. Model calculations were performed on the neutrally stable boundary layer flow. We found that spin has weak effect on the particle dispersion but it shows the significant effect on the horizontal flux compared to the zero-spin model.

회전하는 정사각단면 $90^{\circ}$ 곡덕트 내 내향 난류유동 측정 (Measurement of Inward Turbulent Flows in a Rotating with Square Cross-Section $90^{\circ}$ Duct)

  • 김동철;전건호;최영돈
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 추계학술대회논문집B
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    • pp.627-632
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    • 2000
  • Developing turbulent flows in a rotating 90 degree bend with square cross-section were measured by a hot-wire anemometer. The six orientation hot-wire technique was applied to measured the distributions of 3 mean velocities and 6 Reynolds stress components. Effects of Coriolis and centrifugal forces caused by the curvature and rotation of bend on the mean motion and turbulence structures were experimentally investigated Productive addition of Coriolis and centrifugal forces to the outward radial direction in the entrance region of bend increases the secondary flow intensity according to the rotational speeds. However, after 45 degree of bend, centrifugal force due to the rotation of bend may promote the break down of counter rotating vortex pair into multi-cellular pattern, thereby decreasing the production rate of turbulence energy and Reynolds stresses.

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산업용 교반기의 유동해석용 전/후처리 장치의 개발 (The Development of a Processor for an Industrial Mixer)

  • 김민철;김영규;허남건
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2002년도 학술대회지
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    • pp.627-630
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    • 2002
  • In the present study a mesh generation program is developed for the flow analysis of industrial mixers. With this program one can select various design parameters such as impeller types, vessel type, number of baffles, number of blades, blade pitched angle, stages of impeller, rotational speed etc. Post processing capabilities are also imbedded in the program. Along with brief explanation of the program, examples of flow simulation for various type of mixers by using the program are also presented to show effectiveness of the program. It is expected that this program can be used to understand the effect of design parameters on the performance of particular type of the mixer, and hence to achieve the optimal design.

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개발한 국산화 유압 액셜피스톤모터의 특성실험 (Characteristics Experiment of Domestic Developed Hydraulic Axial Piston Motor)

  • 염만오;이상윤
    • 한국공작기계학회논문집
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    • 제16권5호
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    • pp.70-76
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    • 2007
  • The purpose of this study is to analyze the characteristics of a domestic developed hydraulic axial piston motor. An experimental apparatus was constructed and the output torque, the input oil pressure, the input flow rate, the speed of motor and oil temperature were measured. They were measured under both no load and load conditions. The results are as follows; 1. Motion of motor became steady state conditions after 5 seconds. 2. Output torque of motor was proportional to input oil pressure under both load and unload. 3. Speed of motor decreased with increasing load. 4. Oil temperature was almost constant. The results of this study will offer the basic data in designing and operating hydraulic axial piston motors.

얇은 정사각형 용기 내의 스핀-업 유동에 관한 수치해석적 연구 (A Numerical Study on Spin-up Flows in a Shallow Quadrangular Container)

  • 박재현;서용권
    • 대한기계학회논문집B
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    • 제26권7호
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    • pp.1005-1013
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    • 2002
  • Spin-up is a transient flow phenomenon occurring in a container when it starts to rotate from rest or its rotational speed increases from a low to high value. However, most studies on this subject have been for two-dimensional approximation. In this study, spin-up flows in a shallow rectangular container are analysed by using three-dimensional computation. We compared our results with those obtained by others using basically two-dimensional computation. Effect of two parameters, Reynolds number and liquid depth on the flow evolution is studied. We found that 2-D result is not accurate enough, and the vertical velocity distribution should be assumed of a fourth-order polynomial function for a better comparison.

Design and Prototyping Micro Centrifugal Compressor for Ultra Micro Gas Turbine

  • Hirano, Toshiyuki;Tsujita, Hoshio;Gu, Ronglei;Minorikawa, Gaku
    • International Journal of Fluid Machinery and Systems
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    • 제2권4호
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    • pp.426-430
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    • 2009
  • In order to investigate the design method for a micro centrifugal compressor, which is the most important component of an ultra micro gas turbine, an impeller having the outer diameter of 20mm was designed, manufactured and tested. The designed rotational speed is 500,000 rpm and the impeller has a fully 3-dimensional shape. The impeller was rotated at 250,000 rpm in the present study. The experimental results of the tested compressor with the vaned and the vaneless diffusers were compared. It was found that the vaned diffuser attained the higher flow rate than the vaneless diffuser at the maximum pressure ratio. In addition the maximum pressure ratio was higher for the diffuser having a larger diffuser divergence angle at the high flow rate. These results were compared with those obtained by the prediction method used at the design stage.

축류형 팬의 저소음화에 관한 연구 (A Study on the Noise Reduction of Axial Flow Fan)

  • 오재응;이승종;이상환;이동익;김철환
    • 설비공학논문집
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    • 제7권1호
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    • pp.142-149
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    • 1995
  • Axial fans are very useful cooling devices being widely used in many electric and industrial machinery. However those are often accompanying annoying noise. Many efforts have been devoted in order to reduce the fan noise. In this study, the procedure was devided into two major parts in considering effects of design parameters of axial fan concerned with noise ; the fan theory and the Fukano's fan noise study. By using the fan theory we defined stagger angle, camber angle, blade inlet and outlet angle for studying low noise fan. Then the effects of such angles on the flow rate and static pressure were investigated. By using the Fukano's fan noise theory, the relations of the chord length, the rotational speed and the number of blades vs. fan noise are investigated.

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회전하는 회전체 주위의 축대칭 두꺼운 난류경계층 연구 (Axisymmetric Thick Turbulent Boundary Layer Around a Rotating Body of Revolution)

  • 강신형;황정호
    • 대한조선학회지
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    • 제23권1호
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    • pp.13-22
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    • 1986
  • Axisymmetric turbulent thick boundary layers on a rotating body of revolution are calculated numerically in the paper. Richardson number is introduced to the mixing length to take account of swirl effects on Reynolds stresses. Interactions of the boundary layer and the external potential flow are included by adding the displacement thickness of boundary layers on the original body. Pressure distributions on the body surface are estimated by integrating normal momentum equation across the boundary layer. A model is designed and tested in the wind tunnel. Mean velocities are measured. Through the present study, swirl effects on the thick axisymmetric boundary layer development are considerable in comparison with those of non-totating cases. Rotational motion generally increase boundary layer thickness, axial skin friction coefficients, and form drags. Circumferential flow can be reversed to induce negative skin friction when the section area is reduced.

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