• Title/Summary/Keyword: Secondary Stream Thickness

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Effect of Nozzle Geometry on the Near Field Structure of Under Expanded, Dual, Coaxial Jet (노즐 형상이 부족팽창 동축제트 근접 유동장에 미치는 영향)

  • Lee, Kwon-Hee;Toshiake, Setoguchi;Kim, Heuy-Dong
    • Proceedings of the KSME Conference
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    • 2004.04a
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    • pp.1649-1654
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    • 2004
  • The near field structures of an under-expanded, dual, coaxial, jets issuing from the coaxial nozzles with four different geometries are visualized by using a shadowgraph optical method. Experiments are conducted to investigate the effects of the nozzle-lip thickness, secondary stream thickness, the nozzle pressure ratio and the secondary swirl stream on the characteristics of under-expanded jets. The results show that the presence of secondary annular swirling stream causes the Mach disk to move further downstream and increases its diameter, which decreases with a decrease in the nozzle-lip thickness. The secondary stream thickness has an influence on the location of an annular shock wave.

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Effects of Multi-hole Baffle Thickness on Flow and Mixing Characteristics of Micro Combustor (다공배플 두께가 마이크로 연소기의 유동 및 혼합특성에 미치는 영향)

  • Kim, Won Hyun;Park, Tae Seon
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.41 no.9
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    • pp.623-629
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    • 2017
  • Flow structure and mixing characteristics in a micro combustor with a multi-hole baffle were numerically studied using the Reynolds stress model. The multi-hole baffle has geometrical features to produce multiple three-dimensional vortices inside combustion chamber. When the thickness of the baffle's geometrical factors changes, variations of vortical structures occur variously. Among these vortices, the vortex generated from the fuel stream exerts a critical influence on the mixing enhancement. The three-dimensional vortical structure, in its development state, was strongly dependent on the baffle thickness. In particular, as the baffle thickness decreases to values less than the diameter of the fuel hole, the jet stream in baffle holes changes from the parabolic to saddleback profile type. The sizes of recirculation zones inside combustion chamber and the mixing state were closely affected by the structure of the jet streams.

Experimental Study of Three-Dimensional Turbulent Flow in a $90^{\circ}C$ Rectanglar Cross Sectional Strongly Curved Duct (직사각형 단면을 갖는 $90^{\circ}C$ 급곡관 내의 3차원 난류유동에 관한 실험적 연구)

  • 맹주성;류명석;양시영;장용준
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.15 no.1
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    • pp.262-273
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    • 1991
  • In the present study, the steady, incompressible, isothermal, developing flow in a 90.deg. rectangular cross sectional strongly curved duct with aspect ratio 1:1.5 and Reynolds number of 9.4*10$^{4}$ has been investigated. Measurements of components of mean velocities, pressures, and corresponding components of the Reynolds stress tensor are obtained with a hot-wire anemometer and pitot tube. In general, flow in a curved duct is characterized by the secondary vortices which are driven mainly by centrifugal force-radial pressure gradient imbalance, and the stress field stabilizing effects near the convex wall and destablizing effects close to the concave wall. It was found that the secondary mean velocities attain values up to 39% of the bulk velocity and are largely responsible for the convections of Reynolds stress in the cross stream plane. Therefor upstream of the bend the Reynolds stress are low. Corresponding to the small boundary layer thickness. At successive planes, large values of Reynolds stress were observed near the concave surface and the side wall.

Three-dimensional Numerical Modeling of Fluid Flow and Heat Transfer in Continuously Cast Billets (연속주조 빌렛의 3차원 열 및 유동해석)

  • Lee, Sung-Yoon;Lee, Sang-Mok;Park, Joong-Kil;Hong, Chun-Pyo
    • Journal of Korea Foundry Society
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    • v.20 no.5
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    • pp.290-299
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    • 2000
  • A three-dimensional model was developed in order to simulate heat and fluid flow of a continuous casting billet. The model was coded with the general-purpose CFD program FIDAP, using the finite element method. The present model consists of 2 individual calculation schemes, named model 1 and model 2. Mold region only was calculated to check the pouring stream through submerged nozzle with model 1. Entire region, which consists of mold, secondary cooling, radiation cooling was calculated to predict crater end position, temperature profile and solid shell profile(model 2). Standard $k-{\bullet}\hat{A}$ turbulence model has been applied to simulate the turbulent flow induced by submerged nozzle. Enthalpy method was adopted for the latent heat of solidification. Fluid flow in mushy zone was treated using variable viscosity approach. The more casting speed and superheat increased, the more metallurgical length increased. The shell thickness at the mold exit is proved to be mainly controlled by superheat by the present simulation. It may be concluded that the present model can be successfully applied far the prediction of heat and fluid flow behavior in the continuous casting process.

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