Turbulent Boundary-Layer along a Streamwise Bar of a Rectangular Cross Section Placed on a Flat Plate
スポンサーリンク
概要
- 論文の詳細を見る
Three-dimensional turbulent boundary layer developing along a long streamwise bar of a rectangular cross section (60 mm × 20 mm) placed on a flat plate was investigated experimentally. Two different wall configurations are possible by placing the longer sides of a rectangle perpendicular or parallel to the plate surface. This class of turbulent boundary layers is made complicated by secondary currents which inevitably arise near the streamwise corners. Experimental results obtained for both wall shapes are described mainly concerning isovels, lines of constant turbulence intensity, secondary currents measurements by vortex-meter, distributions of wall shear stress and total drags. Considerations are made on the velocity profiles in a plane of flow symmetry where secondary currents flow toward the wall, and a self-preserving distribution in the outer layer is proposed.
- 一般社団法人日本機械学会の論文
著者
-
Nakamura Ikuo
Faculty Of Engineering Nagoya University
-
Miyata Masafumi
Faculty Of Engineering Nagoya University
-
FURUYA Yoshimasa
Faculty of Engineering, Nagoya University
-
YAMA Yasuhiro
Japan Air Line, Ltd.
-
Furuya Yoshimasa
Faculty Of Engineering Nagoya University
-
Yama Yasuhiro
Japan Air Line Ltd.
-
Nakamura Ikuo
Faculty Of Engineering. Nagoya University
-
Nakamura Ikuo
Faculty Mechanical Engineering Nagoya University
-
FURUYA Yoshimasa
Faculty of Engineering , Nagoya University
関連論文
- Molecular discrimination among taxa of Petunia axillaris complex and P. integrifolia complex based on PolA1 sequence analysis
- Transgenic Phalaenopsis plants with resistance to Erwinia carotovora produced by introducing wasabi defensin gene using Agrobacterium method
- The spanwise non-uniformity of nominally two-dimensional turbulent boundary layer : 4th Report, Uniformalization of flow field and Comparison of various flows
- The spanwise non-uniformity of nominally two-dimensional turbulent boundary layer : 3rd Report, Influence of the streamwise vortices arising from the protrusion
- The spanwise non-uniformity of nominally two-dimensional turbulent boundary layer : 2nd Report Wall shear stress and flow field
- Experiments on the Relatively Thick, Turbulent Boundary Layers on a Rotating Cylinder in Axial Flows : 2nd Report, Flows under Pressure Gradients
- The Structure of a Turbulent Wake Behind a Cruciform Circular Cylinder : 2nd Report, The Streamwise Development of turbulent flow field
- The Structure of a Turbulent Wake behind a Cruciform Circular Cylinder : 1st Report, The Mean Velocity Field
- Turbulent Boundary Layers on plates Roughened by Wires at Equal Intervals
- Turbulent Boundary-Layer along a Streamwise Bar of a Rectangular Cross Section Placed on a Flat Plate
- Turbulent Boundary-Layer along a Streamwise Bar of a Square Cross Section Placed on a Flat Plate
- Laminar Boundary Layer on a Rotating Thin Cylinder in an Axial Flow : Effect of Self-induced Pressure Gradient on Separation
- A Basic Study on a Very Low-Level DC Current Amplifier Using a Switched-Capacitor Circuit(Papers Selected from ITC-CSCC 2004)
- Turbulent Boundary Layers on Wire-Screen Roughnesses
- A Basic Study on Control Command Input Device Using Head Movement for FES System : Availability of Acceleration Sensors(Papers Selected from 2003 International Technical Conference on Circuits/Systems, Computers and Communications(ITC-CSC
- The Loss of Flow in the Conical Diffusers with Suction at the Entrance
- On the Racing Power of Impellers
- The Experiment on the Skewed Boundary Layer on a Rotating Body
- The spanwise non-uniformity of nominally two-dimensional turbulent boundary layer : 1st Report Characteristics of spanwise velocity distribution
- Performance of the Two-Dimensional Diffusers with Suction at the Entrance
- An Experimental Investigation of the Skewed Boundary Layer on a Rotating Body (2nd Report)
- The Rotating Flows in a Vaneless Diffuser Having Two Parallel Discs
- Pressure Recovery Efficiency of Short Conical Diffusers and of Roughened Diffusers
- A Basic Study on Noise Source Modeling for a Very Low-Level DC Current Amplifier(Papers Selected from ITC-CSCC 2004)
- An Automatic Generation of FORTRAN Code for the Finite Difference Method
- Similar Solutions for Boundary Layers on Bodies of Revolution in Swirling Axial Streams