Turbulent Boundary Layer on a Rotating Disk in Infinite Quiescent Fluid
スポンサーリンク
概要
- 論文の詳細を見る
An experimental study of the turbulent flow due to a rotating disk in an infinite quiescent fluid was conducted. Using a single normal- and an inclined-type hot wire, the mean velocity distributions and all six components of Reynolds stress were obtained for various local Reynolds numbers Re_L(=γ^2ω/ν). A log-law region, where the circumferential velocity profile shows a linear variation in a semilogarithmic plot, was observed at Re_L≧4×10^5. The profile in the log-law region at Re_L=1.0×10^6 was in close agreement with that for the flat-plate boundary layer. All components of the turbulence intensity, normalized by the friction velocity, were found to be considerably smaller than those for the flat-plate boundary layer, except very near the wall. The values of the structure parameter a_1 are smaller than those for the flat-plate boundary layer.
- 一般社団法人日本機械学会の論文
- 1994-08-15
著者
-
Itoh Motoyuki
Department Of Mechanical Engineering Nagoya Institute Of Technology
-
Hasegawa Isamu
Suzuka College of Technology
関連論文
- Experimental Study of Rayleigh-Taylor Instability in a Shock Thbe Accompanying Cavity Formation : General Physics
- Acceleration of Water Column and Generation of Large Flow Rate Water Spray by Shock Tube
- Generation of Hypervelocity Liquid Jets Using a Powder Gun and Impact Experiment
- Generation of High-Speed Liquid Jet from a Rectangular Nozzle
- Characteristics of Low-Speed Streaks in the Flow of Drag-Reducing Surfactant Solution
- Further Study of the Generation Technique of High-Speed Liquid Jets and Related Shock Wave Phenomena Using a Helium Gas Gun
- Turbulent Boundary Layer on a Rotating Disk in Infinite Quiescent Fluid
- Viscoelastic Flow Due to a Rotating Disc Enclosed in a Cylindrical Casing : Influence of Aspect Ratio
- Model Experiment, Numerical Simulation and Theoretical Analysis on the Characteristics of a Viscous Micropump Using a Cylindrical Rotor in a Rectangular Duct
- Design and Experiment of a Small High-Speed Liquid Jet Apparatus
- Stage-specific expression of mouse BST-1/BP-3 on the early B and T cell progenitors prior to gene rearrangement of antigen receptor