• 제목/요약/키워드: Annular slit

검색결과 11건 처리시간 0.013초

스파이럴 제트 유동에 미치는 환형 슬릿의 영향에 관한 연구 (The Effect of Annular Slit on a Compressible Spiral Jet Flow)

  • 조위분;백승철;김희동
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 춘계학술대회
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    • pp.2029-2034
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    • 2004
  • Spiral jet is characterized by a wide region of the free vortex flow with a steep axial velocity gradient, while swirl jet is largely governed by the forced vortex flow and has a very low axial velocity at the jet axis. However, detailed generation mechanism of spiral flow components is not well understood, although the spiral jet is extensively applied in a variety of industrial field. In general, it is known that spiral jet is generated by the radial flow injection through an annular slit which is installed at the inlet of a conical convergent nozzle. The present study describes a computational work to investigate the effects of annular slit on the spiral jet. In the present computation, a finite volume scheme is used to solve three dimensional Naver-Stokes equations with RNG ${\kappa}-{\varepsilon}$ turbulent model. The annular slit width and the pressure ratio of the spiral jet are varied to obtain different spiral flows inside the conical convergent nozzle. The present computational results are compared with the previous experimental data. The results obtained obviously show that the annular slit width and the pressure ratio of the spiral jet strongly influence the characteristics of the spiral jets, such as tangential and axial velocities.

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아음속 스파이럴 제트 유동에 관한 기초적 연구 (A Fundamental Study of the Subsonic Spiral Jet)

  • 조위분;김희동
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 추계학술대회
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    • pp.502-507
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    • 2003
  • Spiral jet is characterized by a wide region of the free vortex flow with a steep axial velocity gradient, while swirl jet is largely governed by the forced vortex flow and has a very low axial velocity at the jet axis. However, detailed generation mechanism of spiral flow components is not well understood, although the spiral jet is extensively applied in a variety of industrial field. In general, it is known that spiral jet is generated by the radial flow injection through an annular slit which is installed at the inlet of convergent nozzle. The objective of the present study is to understand the flow characteristics of the spiral jet, using a computational method. A finite volume scheme is used to solve 3-dimensional Navier-Stokes equations with RNG ${\kappa}-{\varepsilon}$ turbulent model. The computational results are validated by the previous experimental data. It is found that the spiral jet is generated by coanda effect at the inlet of the convergent nozzle and its fundamental features are dependent the pressure ratio of the radial flow through the annular slit and the coanda wall curvature.

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A Study on the Flow Characteristics of the Spiral Flow Nozzle with the Width Change of Annular Slit

  • Kim, T.H.;Setoguchi, T.;Lee, Y.W.
    • 한국가시화정보학회지
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    • 제7권1호
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    • pp.14-20
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    • 2009
  • In comparison with previous researches fur swirling flow, the spiral flow self-generated in the spiral flow nozzle has some different characteristics. It is not needed a compulsive tangential momentum to get its velocity component and has long potential core, relatively low swirl ratio, and high focusing ability. In this study, the self-generated mechanism of the spiral flow was clarified and the effect on the width of annular slit on spiral flow characteristics was investigated experimentally and numerically. As a result, the existence of tangential velocity component regardless of a compulsive angular momentum is clarified and the results obtained by experiment have a satisfactory agreement with those by numerical method, quantitatively and qualitatively.

A Study on the Flow Characteristics with the Width of Annular Slit in Spiral Flow Nozzle

  • Kim, T.H.;Setoguchi, T.;Lee, Y.W.
    • 한국가시화정보학회:학술대회논문집
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    • 한국가시화정보학회 2007년도 추계학술대회
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    • pp.143-148
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    • 2007
  • In comparison with previous researches for swirling flow, the spiral flow self-generated in the spiral flow nozzle has some different characteristics. It is not needed a compulsive tangential momentum to get its velocity component and has long potential core, relatively low swirl ratio, and high focusing ability. In this study, the self-generated mechanism of the spiral flow was clarified and the effect on the width of annular slit on spiral flow characteristics was investigated experimentally and numerically. As a result, the existence of tangential velocity component regardless of a compulsive angular momentum is clarified and the results obtained by experiment have a satisfactory agreement with those by numerical method, quantitatively and qualitatively.

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Theoretical and Numerical Study of Cylindrical-vector-mode Radiation Characteristics in Periodic Metallic Annular Slits and Their Applications

  • Kim, Hyuntai;Jeong, Yoonchan
    • Current Optics and Photonics
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    • 제2권5호
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    • pp.482-487
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    • 2018
  • We investigate the radiation characteristics of radially polarized light and azimuthally polarized light through plasmonic subwavelength-scale annular slit (PSAS) structures, by means of both theoretical and numerical methods. Effective-medium theory was utilized to analyze the characteristics of PSAS structures, and the corresponding results showed that PSAS structures can function as a metallic medium for azimuthally polarized light, or as a low-loss dielectric medium for radially polarized light. Numerical calculations based on the finite-element method were also performed, to verify the theoretical analyses. It turned out that the numerical results supported the theoretical results. Moreover, we exploited the PSAS structures in novel nanophotonic elements with dual functionalities that could selectively focus or pass/block incident light, depending on its polarization state. For example, if PSAS structures were implemented in the dielectric region of a metallic Fresnel zone plate, the modified zone plate could function as a blocking element to azimuthally polarized light, yet as a focusing element to radially polarized light. On the contrary, if PSAS structures were implemented in the metallic region of a metallic Fresnel zone plate (i.e. the inverted form of the former), it could function as a focusing element to azimuthally polarized light, yet as a simple transparent element to radially polarized light.

코안다 효과를 이용한 제트 특성에 관한 연구 (A Study on Jet Characteristic using a Coanda Effect in a Constant Expansion Rate Nozzle)

  • 이동원;이삭;김병지;권순범
    • 한국항공우주학회지
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    • 제35권8호
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    • pp.706-713
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    • 2007
  • 코안다 효과를 유발시키기 위해 환상 슬릿과 팽창률이 일정하지 않은 축소 노즐로부터 분사되는 제트의 구조와 환상의 슬릿과 팽창률이 일정한 노즐로부터 분사되는 제트의 구조를 비교 연구하였다. 실험에 있어서 노즐 입구와 출구 직경을 각각 40mm, 20mm로 하였고, 노즐 출구 평균 속도를 90m/s로 하였다. 3축 이송 장치와 스캐닝 밸브 시스템을 이용하여 제트 축 및 반경 방향 압력을 측정하고, 측정된 정압 및 전압으로부터 구한 속도 분포를 비교 검토하였다. 안정성과 수속성이 우수한 제트를 얻기 위해서는 팽창률이 일정하지 않은 노즐보다 팽창률이 일정한 축소 노즐과 환상의 슬릿을 통해 코안다 효과를 이용하여 분사하는 것이 효과적임을 밝혔다. 또한 팽창에 따른 압력 강하도 팽창률이 일정한 노즐의 경우가 상대적으로 더 작게 됨을 알았다.

스파이럴 제트 유동에 미치는 축소노즐 각도의 영향 (The Effect of Convergent Nozzle Angle on a Spiral Jet Flow)

  • 조위분;백승철;김희동
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 추계학술대회
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    • pp.1482-1487
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    • 2004
  • In general the swirl jet is generated by the injected flow that is forced to the tangential direction. A spiral nozzle which is composed of an annular slit and a convergent nozzle, is released the spiral jet that is generated by the radial flow injection through an annular slit. The objective of the present study is to investigate the additional study that is studied a changed the convergent nozzle angle and nozzle length. In the present computation, a finite volume scheme is used to solve three dimensional Navier-Stokes equations with RNG $k-{\varepsilon}$ turbulent model. The convergent nozzle angle and the nozzle length of the spiral nozzle are varied to obtain different spiral flows inside the conical convergent nozzle. The present computational results are compared with the previous experimental data. The results obtained show that the convergent nozzle angle and the nozzle length of the spiral jet strongly influence the characteristics of the spiral jets, such as a tangential and a jet width.

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부스팅 모드에서 IRR(Integral Rocket Ramjet) 초음속 흡입구의 압력진동 감쇄 방안 연구 (A Study of Preventing Pressure Oscillation for Supersonic Inlet of IRR at the Boosting Mode)

  • 박근홍;윤현걸;임진식
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2010년도 제35회 추계학술대회논문집
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    • pp.563-564
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    • 2010
  • IRR의 부스팅 모드 시 흡입구에 발생하는 압력진동을 감쇄하기 위한 방안을 수치적으로 연구하였다. 축대칭 형태의 초음속 흡입구에 slit을 장착하여 유입되는 공기 유량을 줄여가며 흡입구 내부의 압력 진동을 조사하였다. 흡입되는 유량이 감소함에 따라 압력의 진폭은 감소하고 내부 압력의 최댓값 역시 감소하였으며, 주파수는 약간 증가하는 경향을 보였다. 흡입구의 slit을 이용하여 최적화된 압력 진폭과 주파수대를 얻어낼 수 있다면, 이 방안은 IRR의 부스팅 모드 및 천이 모드에서의 안정성을 높이는데 활용될 수 있을 것으로 판단된다.

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Numerical Study of a Novel Bi-focal Metallic Fresnel Zone Plate Having Shallow Depth-of-field Characteristics

  • Kim, Jinseob;Kim, Juhwan;Na, Jeongkyun;Jeong, Yoonchan
    • Current Optics and Photonics
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    • 제2권2호
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    • pp.147-152
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    • 2018
  • We propose a novel bi-focal metallic Fresnel zone plate (MFZP) with shallow depth-of-field (DOF) characteristics. We design the specific annular slit patterns, exploiting the phase-selection-rule method along with the particle swarm optimization algorithm, which we have recently proposed. We numerically investigate the novel characteristics of the bi-focal MFZP in comparison with those of another bi-focal MFZP having equivalent functionality but designed by the conventional multi-zone method. We verify that whilst both bi-focal MFZPs can produce dual focal spots at $15{\mu}m$ and $25{\mu}m$ away from the MFZP plane, the former exhibits characteristics superior to those of the latter from the viewpoint of axial resolution, including the axial side lobe suppression and axial DOF shallowness. We expect the proposed bi-focal MFZP can readily be fabricated with electron-beam evaporation and focused-ion-beam processes and further be exploited for various applications, such as laser micro-machining, optical trapping, biochemical sensing, confocal sensing, etc.