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Study of Spiral Flow Generated through an Annular Slit 被引量:1

Study of Spiral Flow Generated through an Annular Slit
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摘要 The effect of pressurized air inlets in the reservoir upstream of the annular slit on characteristics of the axial and tangential velocity components is investigated numerically, and the mechanism of occurrence of spiral nozzle flow is clarified. In simulations, Unified Platform for Aerospace Computational Simulation (UPACS) is used. The governing equations under consideration are the unsteady compressible Navier - Stokes. A second-order finite volume scheme with MUSCL (Roe scheme) is used to discretize the spatial derivatives, and a second order-central difference scheme for the viscous terms, and a MFGS (Matrix Free Gauss Seidel) is employed for time integration. Spalart-Allmaras model was used as a turbulence model. The results obtained are compared with velocity distributions in the experiment measured by the two-component fiber optic laser Doppler velocimeter system. The existence of discrete pressurized air inlets that leads to the occurrence of asymmetrical characteristics is a very important factor for the formation of spiral flow. The effect of pressurized air inlets in the reservoir upstream of the annular slit on characteristics of the axial and tangential velocity components is investigated numerically, and the mechanism of occurrence of spiral nozzle flow is clarified. In simulations, Unified Platform for Aerospace Computational Simulation (UPACS) is used. The governing equations under consideration are the unsteady compressible Navier - Stokes. A second-order finite volume scheme with MUSCL (Roe scheme) is used to discretize the spatial derivatives, and a second order-central difference scheme for the viscous terms, and a MFGS (Matrix Free Gauss Seidel) is employed for time integration. Spalart-Allmaras model was used as a turbulence model. The results obtained are compared with velocity distributions in the experiment measured by the two-component fiber optic laser Doppler velocimeter system. The existence of discrete pressurized air inlets that leads to the occurrence of asymmetrical characteristics is a very important factor for the formation of spiral flow.
出处 《Journal of Thermal Science》 SCIE EI CAS CSCD 2005年第2期97-102,共6页 热科学学报(英文版)
关键词 旋转喷嘴流 柯恩达效应 渐缩喷嘴 环形裂缝 计算机仿真 spiral nozzle flow, Coanda effect, convergent nozzle, annular slit, simulation.
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  • 1Horii,K,Matsumae,Y,Ohsumi,K,et al.Novel Optical Fiber Installation by Use of Spiral How[].Journal of Fluids Engineering Transactions of the ASME.1992
  • 2Horii,K,Sawazaki,H,Matsumae,Y,et al.New Continuous System for Dispersion and Encapsulation of Submicron Powders Using Spiral Flow[].ASME FED.1990
  • 3Bhagwat,M J,Leishman,J G.Correlation of Helicopter Rotor Tip Vortex Measurements[].AIAA Journal.2000
  • 4Horii,K,Matsumae,Y,Cheng,X M,et al.Focusing Phenomena and Stability of Spiral-Flow Jet[].Trans Japan Soc Aero Space Sci.1991
  • 5Ueda,H,Sakai,M,Horii,K,et al.Study of Swirling Pneumatic Transport of Granule in a Horizontal Pipe.Trans. Jpn. Soc[].Mechanical Engineering.2001
  • 6Miyazaki,K,Chen,G,Kudamatsuo,J et al.High-Efficiency Soil Transportation with Spiral Airflow[].Japan Soc Aero Space Sci.1999
  • 7Horii,K,Matsumae,Y,Cheng,X M,et al.A Study of Spiral Flow (Part 4) The Effect of Radial Reynolds Number of Spiral Flow on Plasma Deposition of Pipe[].Trans Japan Soc Aero Space Sci.1990
  • 8Yamane,T,Yamamoto,K,Enomoto,S,et al.Current Status of Common CFD Platform-UPACS, In: Proc[].of Aerospace Numerical Simulation Symposium Tokyo Japan.2000

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