The transition from Laminar to turbulent flow were made by two-dimensional roughness element (cylindrical) affached to the flat plate. The experiments were made on the boundary layer along a flat plate in a two-dimensional wind tunnel. The purpose of this experiments is to make the fundamental data, and discuss the effect of the ratio of its roughness element diameter K to the displacement thickness δ^* on the local value of the heat transfer coefficients in the transition region. When k/δ^* is large. large Value of the heat transfer coefficient is obtained at the place affached the element, and its Value is larger than that of the turbulent flow in a flat plat
An investigation has been conducted at a Mach number of 3 of the effect of turbulence level and sand...
Laminar-turbulent transition in compressible, high-speed boundary layers is currently not well under...
The transition characteristics and the boundary layer development behind an isolated spherical rough...
SIGLEAvailable from British Library Document Supply Centre-DSC:DXN004775 / BLDSC - British Library D...
This investigation was carried out to clarify the effects of two dimensional thin wire, placed withi...
The effect of the location of transition on the heat transfer to the turbulent incompressible bounda...
The heat transfer enhancement was experimentally investigated over the flat, concave, convex, and ri...
In order to assess the direct influence of surface roughtness upon heat transfer andits indirect eff...
Laminar turbulent transition is known for a long time as a critical phenomenon influencing the therm...
Experimental results are presented to document hydrodynamic and thermal development of flat-plate bo...
In the context of the ongoing research regarding boundary layer transition, this project aims to stu...
Experiments were performed in two low‐turbulence wind tunnels (u∞′ < 0.1%) to determine the effects ...
The laminar and turbulent regimes of a boundary layer on a flat plate are often represented with sep...
The laminar boundary layer and the position of the transition point are investigated on a heated fla...
The laminar boundaxy layer and the position of the transition point were investigated on a heated fl...
An investigation has been conducted at a Mach number of 3 of the effect of turbulence level and sand...
Laminar-turbulent transition in compressible, high-speed boundary layers is currently not well under...
The transition characteristics and the boundary layer development behind an isolated spherical rough...
SIGLEAvailable from British Library Document Supply Centre-DSC:DXN004775 / BLDSC - British Library D...
This investigation was carried out to clarify the effects of two dimensional thin wire, placed withi...
The effect of the location of transition on the heat transfer to the turbulent incompressible bounda...
The heat transfer enhancement was experimentally investigated over the flat, concave, convex, and ri...
In order to assess the direct influence of surface roughtness upon heat transfer andits indirect eff...
Laminar turbulent transition is known for a long time as a critical phenomenon influencing the therm...
Experimental results are presented to document hydrodynamic and thermal development of flat-plate bo...
In the context of the ongoing research regarding boundary layer transition, this project aims to stu...
Experiments were performed in two low‐turbulence wind tunnels (u∞′ < 0.1%) to determine the effects ...
The laminar and turbulent regimes of a boundary layer on a flat plate are often represented with sep...
The laminar boundary layer and the position of the transition point are investigated on a heated fla...
The laminar boundaxy layer and the position of the transition point were investigated on a heated fl...
An investigation has been conducted at a Mach number of 3 of the effect of turbulence level and sand...
Laminar-turbulent transition in compressible, high-speed boundary layers is currently not well under...
The transition characteristics and the boundary layer development behind an isolated spherical rough...