DocumentCode
1720061
Title
Thermal-control technique to improve flow characteristics over curved and rotating surfaces
Author
Yurchenko, Nina
Author_Institution
Inst. of Hydromech., Acad. of Sci., Kiev, Ukraine
fYear
2001
fDate
8/1/2001 12:00:00 AM
Firstpage
378
Lastpage
385
Abstract
One of the particular features of flows with available large-scale vortices deals with specific mechanisms of fluid transport. Thus modifying vortex scales, one can affect processes of heat and momentum transfer near a wall. In this connection, experiments were carried out to demonstrate how a scale of a fluid motion can be changed both in transitional and turbulent boundary layers using an imposed spanwise-regular temperature distribution over the surface. This method was tested for flows under body forces where counter-rotating streamwise vortices are an inherent flow feature. An active mode of vortex generation is realized due to two independent variables, spanwise scale of induced vortices and temperature gradient over the surface that can be adjusted to current flow conditions. Velocity fields and spectrum redistribution in boundary layers with embedded streamwise vortices show efficiency and prospects of the proposed method to control turbulent transport
Keywords
Navier-Stokes equations; boundary layer turbulence; flow control; heating; laminar to turbulent transitions; subsonic flow; temperature distribution; vortices; Navier-Stokes equations; active mode; body forces; centrifugal forces; compressible subsonic boundary layers; counter-rotating streamwise vortices; curved surfaces; embedded streamwise vortices; flow control similarity principle; imposed spanwise-regular temperature distribution; laminar turbulent transition; large-scale motion; large-scale vortices; rotating surfaces; spanwise scale; spectrum redistribution; temperature gradient; thermal-control technique; transitional boundary layers; turbine blade; turbulent boundary layers; turbulent transport control; velocity fields; vortex generation; vortex visualization; Blades; Engines; Heat transfer; Large-scale systems; Liquid crystal displays; Temperature distribution; Testing; Turbines; Velocity control; Visualization;
fLanguage
English
Publisher
ieee
Conference_Titel
Instrumentation in Aerospace Simulation Facilities, 2001. 19th International Congress on ICIASF 2001
Conference_Location
Cleveland, OH
Print_ISBN
0-7803-7022-8
Type
conf
DOI
10.1109/ICIASF.2001.960273
Filename
960273
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