• 제목/요약/키워드: Interaction of jets

검색결과 52건 처리시간 0.021초

돌출 발열블록 표면에서의 배열 충돌제트에 의한 열전달 특성 (Heat transfer characteristics of multiple slot jets at the surface of protruding heated blocks)

  • 정인기;박시우;홍성호
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 추계학술대회논문집B
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    • pp.274-279
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    • 2001
  • An experimental investigation of heat transfer characteristics at the surface of two-dimensional protruding heated blocks using confined impinging multiple slot jets has been performed. The effects of jet-to-jet distances(S=16B, 24B), dimensionless nozzle-to-block distances(H/B=2, 6) and jet Reynolds numbers(Re=2000, 3900, 5800, 7800) on the local and average heat transfer coefficients have been examined with five isothermally heated blocks at streamwise block spacing(p/w=1). To clarify local heat transfer characteristics, naphthalene sublimation technique was used. From the results, it was found that the local and average heat transfer of heated blocks increases with decreasing jet-to-jet distance and increasing jet Reynolds number. Measurements of local heat transfer coefficients have given an indication of the nature of the interaction between jets and of the uniformity of heat transfer obtainable with various arrangements. In the case of S/B=16, H/B=6 and Re=7800, maximum average Nusselt number of overall blocks was obtained.

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Experimental and Computational Study on Separation Control Performance of Synthetic Jets with Circular Exit

  • Kim, Minhee;Lee, Byunghyun;Lee, Junhee;Kim, Chongam
    • International Journal of Aeronautical and Space Sciences
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    • 제17권3호
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    • pp.296-314
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    • 2016
  • This paper presents experimental and computational investigations of synthetic jets with a circular exit for improving flow control performance. First, the flow feature and vortex structure of a multiple serial circular exit were numerically analyzed from the view point of flow control effect under a cross flow condition. In order to improve separation control performance, experimental and numerical studies were conducted according to several key parameters, such as hole diameter, hole gap, the number of hole, jet array, and phase difference. Experiments were carried out in a quiescent condition and a forced separated flow condition using piezoelectrically driven synthetic jets. Jet characteristics were compared by measuring velocity profiles and pressure distributions. The interaction of synthetic jets with a freestream was examined by analyzing vortical structure characteristics. For separation control performance, separated flow over an airfoil at high angles of attack was employed and the flow control performance of the proposed synthetic jet was verified by measuring aerodynamic coefficient. The circular exit with a suitable hole parameter provides stable and persistent jet vortices that do beneficially affect separation control. This demonstrates the flow control performance of circular exit array could be remarkably improved by applying a set of suitable hole parameters.

배열 슬롯제트의 노즐간격 변화에 따른 충돌면에서의 열전달 특성 (Heat transfer characteristics of impinging flat plate of multiple slot jets by changing of jet-to-jet distance)

  • 정인기;박시우;홍성호;고완욱
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집D
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    • pp.534-539
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    • 2001
  • An experimental investigation of heat transfer characteristics on confined jet impinging plate using multiple slot jets has been performed. The effects of jet Reynolds numbers(Re=2000, 3950, 5900, 7900), dimensionlesss slot-to-plate distances(H/B=2, 4, 6, 8) and jet-to-jet distances(S=16B, 20B, 24B, 30B) on the local and average heat transfer coefficients have been examined. To clarify local heat transfer characteristics, naphthalene sublimation technique were used. From the experimental results, it was found that the local and average heat transfer rates increase with increasing jet Reynolds number. Measurements of local heat transfer coefficients produced by multiple of slot jets have given an indication of the nature of the interaction between jets and of the uniformity of heat transfer obtainable with various arrangements. At S/B=20, Re=7900 and H/B=6, maximum average Nusselt number is obtained.

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꼭지각이 $60^{\cire}$인 쐐기에 충돌하는 초음속 제트의 공기역학적 특성 (Aerodynamic Characteristics of Supersonic Jets Impinging on $60^{\cire}$ Wedge)

  • 박종호;이택상;김윤곤
    • 한국추진공학회지
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    • 제8권1호
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    • pp.8-15
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    • 2004
  • 제트 편향기 설계를 위한 기초 자료로 활용하기 위해 꼭지각 $60^{\cire}$인 쐐기에 충돌하는 초음속 제트에 대해 연구하였다. 초음속 제트가 쐐기에 충돌할 때 발생되는 주요 특징은 충격파 간섭과 유동의 박리현상이다. 초음속 유동장치를 이용하여 유동가시화, 표면압력분포, 등압력분포를 측정하고 실험결과와의 비교 및 검증을 위해 유동해석을 하였다 주요변수로는 과소팽창비, 노즐출구에서 꼭지점까지 거리, 설계마하수를 고려하였다. 쐐기 충격파가 이격 또는 부착되는 조건을 확인하였으며 유동장에 지배적 영향을 끼치는 인자는 자유제트의 강도, 쐐기 충격파와 배럴 충격파의 간섭에 의해 형성되는 충격파 패턴임을 알 수 있었다.

성형작약제트와 표적 상호작용 해석 방법론 (Methodologies for Analyzing Interaction between Shape Charge Jets and Targets)

  • 강민아;박성준;;;문세훈
    • 한국시뮬레이션학회논문지
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    • 제31권3호
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    • pp.11-21
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    • 2022
  • 국과연은 물자표적에 대한 취약성 해석 모델인 AVEAM-MT(ADD Vulnerability and Effectiveness Assessment Model for Materiel Target)를 개발하고 있다. 이 모델에는 성형작약제트와 표적 간 상호작용을 해석하기 위해 두 가지 방법이 적용되었다. 그중 한 방법은 표적 부품으로 침투를 신속하게 계산하기 위해 Fireman-Pugh 방법을 개량한 경험적 모델이다. 다른 하나는 Walker-Anderson 침투모델을 성형작약제트에 적용할 수 있도록 개량한 물리기반 모델인 ADD-TSC(ADD Tandem Shaped Charge)이다. 이 논문에서는 이 두 방법을 간략히 기술하고, 경험식 방법과 물리기반 모델의 잔류침투성능 예측 결과를 비교한다. 또한 물리기반 모델이 예측한 침투성능과 문헌에서 찾은 실험 결과를 비교한다. 비교 결과는 두 방법 모두 AVEAM-MT와 같은 짧은 시간에 상당한 양의 반복적인 피해해석 시뮬레이션 수행이 요구되는 취약성 해석 모델에 탑재되어 고속 계산 또는 상대적으로 높은 충실도 계산에 유용하게 사용될 수 있음을 보인다.

플라즈마 합성제트를 이용한 사각 실린더 유동의 제어 (CONTROL OF SQUARE CYLINDER FLOW USING PLASMA SYNTHETIC JETS)

  • 김동주;김경진
    • 한국전산유체공학회지
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    • 제17권2호
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    • pp.85-92
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    • 2012
  • Flows over a square cylinder with and without plasma actuation are numerically investigated to see whether plasma actuation can effectively modify vortex shedding from the cylinder and reduce the drag and lift fluctuations. In this study, a plasma synthetic jet actuator is mounted on the rear side of cylinder as a means of direct-wake control. The effect of plasma actuation is considered by adding a momentum forcing term in the Navier-Stokes equations. Results show that the reduction of mean drag and lift fluctuations is obtained for both steady and unsteady actuation. However, the steady actuation is better than the unsteady one in terms of mean drag as well as drag fluctuations. With the strong steady actuation considered, the interaction of two separating shear layers from rear corners is effectively weakened due to the interference of synthetic jets. It results in a merging of synthetic-jet and shear-layer vortices and the increase of vortex shedding frequency. On the other hand, the unsteady actuation generates pulsating synthetic jets in the near wake, but it does not change the vortex shedding frequency for the actuation frequencies considered in this study.

원뿔에 충돌하는 초음속 제트에 관한 연구 (A Study of Supersonic Jets Impinging on Axisymmetric Cone)

  • 박종호;이택상;김윤곤
    • 한국항공우주학회지
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    • 제31권7호
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    • pp.26-31
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    • 2003
  • 수직 이착륙기나 로켓 등을 발사시킬 때 사용되는 제트 편향기 설계를 위한 기초 자료를 얻기 위해 축대칭 원뿔에 충돌하는 초음속 제트에 대한 연구를 수행하였다. 본 논문에서는 충격파 간섭 또는 전단층에 의한 박리 등과 같은 유동 현상을 분석하기 위해 쉬리렌 장치를 이용한 유동가시화, 표면압력분포 등을 측정하였으며, 수치해석을 통해 실험결과와 비교, 검증하였다. 유동은 원뿔 충격파와 배럴 충격파 사이에서 간섭으로 인해 발생되는 충격파 패턴이었으며, 자유제트의 구조에 따라 다양한 형상을 나타내며 표면 압력분포에 크게 영향을 미친다.

동축제트의 와류주파수 및 혼합특성에 대한 수치해석 (NUMERICAL STUDY ON THE CHARACTERISTICS OF VORTEX FREQUENCY AND LAMINAR MIXING OF A PASSIVE SCALAR IN COAXIAL JET FLOWS)

  • 김원현;박태선
    • 한국전산유체공학회지
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    • 제14권3호
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    • pp.49-55
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    • 2009
  • This study focuses on the near-field vortical structure and dynamics of coaxial jets. The characteristics of laminar flow and mixing in coaxial jets are investigated using a unsteady flow simulation. In order to analyze the geometric effects on the vortical structure, several cases of different configurations are selected for various values of the velocity ratio of inner jet to outer jet. From the result, it is confirmed that the flow mixing is promoted by the development of vortical structure and the interaction between inner jet and outer jet. This feature is strongly related to the vortex frequency in the shear-layers. The vortex frequency depends on the velocity ratio and the lip thickness of inner nozzle, but the outer pipe length has no effect on the frequency variation.

Experimental Study of Film Cooling Behaviors at a Cylindrical Leading Edge

  • Kim S. M.;Kim Youn-J.
    • 한국가시화정보학회:학술대회논문집
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    • 한국가시화정보학회 2002년도 추계학술대회 논문집
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    • pp.81-84
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    • 2002
  • Dispersion of coolant jets in a film cooling flow field is the result of a highly complex interaction between the film cooling jets and the mainstream. In order to investigate the effect of blowing ratios on the film cooling of turbine blade, cylindrical body model was used. Mainstream Reynolds number based on the cylinder diameter was $7.1\;\times\;10^4$. The free-stream turbulence intensity kept at $5.0\%$ by using turbulence grid. The effect of coolant flow rates was studied for blowing ratios of 0.9, 1.3 and 1.6, respectively. The temperature distribution of the cylindrical model surface is visualized by infrared thermography (IRT). Results show that the film-cooling performance may be significantly improved by controlling the blowing ratio. As blowing ratio increases, the adiabatic film cooling effectiveness is more broadly distributed and the area protected by coolant increases. The mass flow rate of the coolant through the first-row holes is less than that through the second-row holes due to the pressure variation around the cylinder surface.

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오목한 반구면의 Jet Impingement/Effusion Hole 주변 유동 특성에 대한 실험과 시뮬레이션의 비교 (Comparison of Experimental and Simulation Results for Flow Characteristics around Jet Impingement/Effusion Hole in Concave Hemispherical Surface)

  • 윤성지;서희림;염은섭
    • 한국가시화정보학회지
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    • 제20권2호
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    • pp.28-37
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    • 2022
  • Flow characteristics of jet impingement over concave hemispherical surface with effusion cooling holes is relatively more complex than that of a flat surface, so the experimental validation for computational fluid dynamics (CFD) results is important. In this study, experimental results were compared with simulation results obtained by assuming different turbulence models. The vortex was observed in the region between the central jets where the recirculation structure appeared. The different patterns of vorticity distributions were observed for each turbulence models due to different interaction of the injected jet flow. Among them, the transition k-kl-ω model predicted similarly not only the jet potential core region with higher velocity, but also the recirculation region between the central jets. From the validation, it may be helpful to accurately predict heat and mass transfer in jet impingement/effusion hole system.