• 제목/요약/키워드: Separation Layer

검색결과 804건 처리시간 0.026초

비정상 층류 경계층 박리에 의한 유동 소음 (Aeroacoustic Noise Generation in Unsteady Laminar Boundary-layer Separation)

  • 최효원;문영준
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 추계학술대회논문집B
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    • pp.300-305
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    • 2001
  • The unsteady flow structure and the related noise generation, which are caused by the separation of a two-dimensional, incompressible, laminar boundary-layer on the flat plate under the influence of local adverse pressure gradient, are numerically examined. The characteristic lines of the wall pressure are examined to understand the unsteady behavior of vortex shedding near the reattachment point of the separation bubble. Also, the generation and propagation of the vortex-induced noise in the separated boundary-layer are calculated by the method of computational aero-acoustics (CAA), and the effects of Reynolds number, Mach number and the strength of the adverse pressure gradient on the unsteady flow and noise characteristics are examined.

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INVESTIGATION ON CRITERION OF SHOCK-INDUCED SEPARATION IN SUPERSONIC FLOWS

  • Heuy-Dong KIM
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 1995년도 제5회 학술강연회논문집
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    • pp.69-83
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    • 1995
  • A great number of experimental data indicating shock-induced separation(SIS) in internal or external supersonic flows were reviewed to make clear the mechanism of SIS and to present the criterion of turbulent boundary layer separation. The interesting conclusions were obtained for the considerably wide range of flow geometries that the incipient separation is almost independent of the flow geometries, and that it is relatively unaffected by changes in gas specific heat, and boundary layer Reynolds number, Furthermore, the pressure rise necessary to separate boundary layer in external flows was found to be applicable to SIS in overexpanded propulsion nozzles. This is due to the fact that the SIS phenomenon caused by the interaction between shock waves and turbulent boundary layers is processed through a supersonic deceleration. This is, the SIS in almost all of interacting flow fields is governed by the concept of free interaction, and criterion of SIS is only a Function of upstream Mach number.

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Self-excited Variability of the East Korea Warm Current: A Quasi-Geostyophic Model Study

  • Lee, Sang-Ki
    • Journal of the korean society of oceanography
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    • 제34권1호
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    • pp.1-21
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    • 1999
  • A two-layer quasi-geostrophic numerical model is used to investigate the temporal variability of the East Korea Warm Current (EKWC), especially the separation from the Korean coast and the generation of warm eddies. An attention is given on the active role of the nonlinear boundary layer process. For this, an idealized flat bottom model of the East Sea is forced with the annual mean wind curl and with the inflow-outflow specified at the Korea (Tsushima) and Tsugaru Straits. Two types of separation mechanisms are identified. The first one is influenced by the westward movement of the recirculating leg of the EKWC (externally driven separation),the second one is solely driven by the boundary layer dynamics (internally driven separation). However, these two processes are not independent, and usually coexist. It is hypothesized that 'internally driven separation' arises as the result of relative vorticity production at the wall, its subsequent advection via the EKWC, and its accumulation up to a critical level characterized by the separation of the boundary flow from the coast. It is found that the sharp southeastern corner of the Korean peninsula provides a favorable condition for the accumulation of relative vorticity. The separation of the EKWC usually accompanies the generation of a warm eddy with a diameter of about 120 km. The warm eddy has a typical layer-averaged velocity of 0.3 m/s and its lifespan is up to a year. In general, the characteristics of the simulated warm eddy are compatible with observations. A conclusion is therefore drawn that the variability of the EKWC is at least partially self-excited, not being influenced by any sources of perturbation in the forcing field, and that the likely source of the variability is the barotropic instability although the extent of contribution from the baroclinic instability remains unknown. The effects of the seasonal wind curl and inflow-outflow strength are also investigated.

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저 레이놀즈수에서 정지된 에어포일의 경계층 및 근접 후류 가시화 연구 (Visualization Study on the Boundary Layer and Near-Wake of a Stationary Airfoil at Low Reynolds Numbers)

  • 양재훈;장조원
    • 한국가시화정보학회지
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    • 제4권2호
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    • pp.44-50
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    • 2006
  • A visualization study on the boundary layer and near-wake of an NACA 0012 airfoil was con-ducted in order to investigate the influence of boundary layer behavior on the near-wake at low Reynolds numbers. The present study is investigated at static angles of attack ${\alpha}=0^{\circ},\;3^{\circ},\;6^{\circ}$ and $Re=2.3{\times}10^4,\;3.3{\times}10^4,\;4.8{\times}10^4$ by using a smoke-wire technique. The results of this study show that the laminar boundary layer on the airfoil surface is attached to the surface at ${\alpha}=0^{\circ}$, and that laminar separation of boundary layer on the airfoil surface occurs at ${\alpha}=3^{\circ}$. Furthermore, reattachment of the boundary layer occurs in the case of ${\alpha}=6^{\circ}$. In the current study, the location of the laminar separation point moves upstream as the Reynolds number and the angle of attack increase.

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Effect of Reynolds number on compressible convex-corner flows

  • Chung, Kung-Ming;Chang, Po-Hsiung;Chang, Keh-Chin
    • Advances in aircraft and spacecraft science
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    • 제1권4호
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    • pp.443-454
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    • 2014
  • An experimental study was conducted to investigate the effect of Reynolds number on compressible convex-corner flows, which correspond to an upper surface of a deflected flap of an aircraft wing. The flow is naturally developed along a flat plate with two different lengths, resulting in different incoming boundary layer thicknesses or Reynolds numbers. It is found that boundary layer Reynolds number, ranging from $8.04{\times}10^4$ to $1.63{\times}10^5$, has a minor influence on flow expansion and compression near the corner apex in the transonic flow regime, but not for the subsonic expansion flow. For shock-induced separated flow, higher peak pressure fluctuations are observed at smaller Reynolds number, corresponding to the excursion phenomena and the shorter region of shock-induced boundary layer separation. An explicit correlation of separation length with deflection angle is also presented.

Monitoring of phase separation between silk fibroin and sericin using various dye system

  • Kwak, Hyo Won;Lee, Ki Hoon
    • International Journal of Industrial Entomology and Biomaterials
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    • 제30권1호
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    • pp.1-5
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    • 2015
  • Understanding the interactions between fibroin and sericin is crucial in solving the mechanism of silk spinning. In this study, various commercially available dyes were used to monitor the interface between fibroin and sericin during the gelation of fibroin. The phase separation between fibroin and sericin could be observed by the addition of azo dyes over a certain molecular weight. Furthermore, the addition of the dyes to the sericin layer showed vivid phase separation over addition to the fibroin layer.

경사충격파 박리유동 제어를 위한 초음속 진동제트 분출위치의 영향성 연구 (A Study of the Influence of the Injection Location of Supersonic Sweeping Jet for the Control of Shock-Induced Separation)

  • 박상훈;이열
    • 한국항공우주학회지
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    • 제50권11호
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    • pp.747-754
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    • 2022
  • 유체진동기에서 분출되는 초음속 진동제트를 이용하여 충격파에 의한 경계층 박리유동을 제어하는 실험적 연구가 이루어졌다. 유체진동기의 위치와 제어압력의 변화가 경사충격파에 의하여 발생되는 경계층 박리유동의 특성에 미치는 영향이 관찰되었고, 이를 위하여 고속 슐리렌, 표면유동가시화, 벽압력 측정, 그리고 정밀 피토관 측정 기법이 적용되었다. 본 연구의 초음속 진동제트의 박리유동 제어 특성은 공기제트 와류를 이용한 기존 제어기법과 정량적으로 비교 분석되었다.

Continuous and discontinuous contact problem for a layered composite resting on simple supports

  • Birinci, Ahmet;Erdol, Ragip
    • Structural Engineering and Mechanics
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    • 제12권1호
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    • pp.17-34
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    • 2001
  • The frictionless contact problem for a layered composite which consists of two elastic layers having different elastic constants and heights resting on two simple supports is considered. The external load is applied to the layered composite through a rigid stamp. For values of the resultant compressive force P acting on the stamp vertically which are less than a critical value $P_{cr}$ and for small flexibility of the layered composite, the continuous contact along the layer - the layer and the stamp - the layered composite is maintained. However, if the flexibility of the layered composite increases and if tensile tractions are not allowed on the interface, for P > $P_{cr}$, a separation may be occurred between the stamp and the layered composite or two elastic layers interface along a certain finite region. The problem is formulated and solved for both cases by using Theory of Elasticity and Integral Transform Technique. Numerical results for $P_{cr}$, separation initiation distance, contact stresses, distances determining the separation area, and the vertical displacement in the separation zone between two elastic layers are given.

방향계 폴리에테르이미드막의 물-알콜 혼합액의 투과증발 특성에 관한 연구 : II.skin layer의 density변화에 의한 물-이소프로판올 혼합액의 투과증발 (Study on the Pervaporation Characteristic of Water-alcohol Mixtures through Aromatic Polyetherimide Membranes : II. the Pervaporation of Water-isopropanol Mixtures by the Density Change of Skin Layer)

  • 김상균;제갈종건;이규호
    • 공업화학
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    • 제8권5호
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    • pp.853-859
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    • 1997
  • 표면층에 치밀층 구배 구조를 갖는 비대칭 폴리에테르이미드막에 대하여 치밀 구조층의 화학적 개질을 통한 막 형태의 변화와 물/이소프로판올 혼합액의 투과증발 거동을 연구하였다. 치밀 정도는 증발 시간에 의해 조절되었고, 증발 시간이 0분에서 4분으로 증가되었을 때, 투과량은 감소하였고, 선택도는 증가하였다. 또한, 수산화나트륨 용액으로 개질 된 폴리에테르이미드막을 통한 투과증발 거동은, 치밀 표면층의 개질 시간이 증가될수록 선택성은 증가하였고, 투과량은 감소하였다. 전자현미경으로 확인된 형태 변화는 개질 시간의 증가에 따라 치밀 표면층의 density 증가를 보여주었고, 이러한 결과는 위의 관찰들과 일치하였다.

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PREPARATION OF POLY(ETHYLENE-CO-VINYL ALCOHOL) MEMBRANE VIA THERMALLY INDUCED PHASE SEPARATION

  • Matsuyama, Hideto;Shang, Mengxian;Teramoto, Masaaki
    • 한국막학회:학술대회논문집
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    • 한국막학회 2004년도 Proceedings of the second conference of aseanian membrane society
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    • pp.74-77
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    • 2004
  • Porous membranes were prepared via thermally induced phase separation (TIPS) of (ethylene-co-vinyl alcohol) (EVOH)/glycerol mixtures. The liquid-liquid (L-L) phase boundaries are shifted to higher temperature when the ethylene contents in EVOH increase. Moreover, the kinetic study proved that the growth of droplets formed by the general liquid-liquid (L-L) phase separation obeyed a power-law scaling relationship in the later stage of spinodal decomposition (SD). A new phase separation mechanism was presented, in which the L-L phase separation could be resulted from the crystallization. The hollow fiber membranes were prepared. The membranes showed asymmetric structures with skin layer near the outer surface, the larger pores just below the skin layer and the smaller pores near the inner surface. The effect of ethylene content (EC) in EVOH, cooling water bath temperature and take-up speed on membrane performance was investigated.

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