Author: Larry Edward Seeley
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 486
Book Description
An Experimental Investigation of Laminar and Turbulent Flow Around a Sphere at Intermediate Reynolds Numbers
Author: Larry Edward Seeley
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 486
Book Description
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 486
Book Description
Experimental Investigation of Turbulent Flows Around a Sphere
Author: Vukman Bakić
Publisher:
ISBN: 9783892206217
Category : Hydrodynamics
Languages : en
Pages : 82
Book Description
Publisher:
ISBN: 9783892206217
Category : Hydrodynamics
Languages : en
Pages : 82
Book Description
Numerical and Experimental Investigation of Flow Past a Sphere Up to a Reynolds Number of 300
Author: Timothy A. Johnson
Publisher:
ISBN:
Category :
Languages : en
Pages : 394
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 394
Book Description
Experimental Investigation of Turbulent Boundary Layer with Uniform Blowing at Moderate and High Reynolds Numbers
Author: Gazi Hasanuzzaman
Publisher: Cuvillier
ISBN: 9783736975583
Category :
Languages : en
Pages : 180
Book Description
Experimental investigation in turbulent boundary layer flows represents one of the canonical geometries of wall bounded shear flows. Utmost relevance of such experiments, however, is applied in the engineering applications in aerospace and marine industries. In particular, continuous effort is being imparted to explore the underlying physics of the flow in order to develop models for numerical tools and to achieve flow control. Flow control experiments have been widely investigated since 1930's. Several flow control technique has been explored and have shown potential benefit. But the choice of control technique depends largely on the boundary condition and the type of application. Hence, friction drag of subsonic transport aircraft is intended to be reduced within the scope of this Ph. D. topic. Therefore, application of active control method such as microblowing effect in the incompressible, zero pressure gradient turbulent boundary layer was investigated. A series of experiments have been performed in two different wind tunnel facilities. Wind tunnel from Department of Aerodynamics and Fluid Mechanics (LAS) was used for the measurements for moderate Reynolds number range in co-operation with the wind tunnel from Laboratoire de M ́ecanique de Feiret Lille for large Reynolds number range. Measurements are conducted with the help of state-of-the-art techniques such as Laser Doppler Anemometry, Particle Image Velocimetry and electronic pressure sensors.
Publisher: Cuvillier
ISBN: 9783736975583
Category :
Languages : en
Pages : 180
Book Description
Experimental investigation in turbulent boundary layer flows represents one of the canonical geometries of wall bounded shear flows. Utmost relevance of such experiments, however, is applied in the engineering applications in aerospace and marine industries. In particular, continuous effort is being imparted to explore the underlying physics of the flow in order to develop models for numerical tools and to achieve flow control. Flow control experiments have been widely investigated since 1930's. Several flow control technique has been explored and have shown potential benefit. But the choice of control technique depends largely on the boundary condition and the type of application. Hence, friction drag of subsonic transport aircraft is intended to be reduced within the scope of this Ph. D. topic. Therefore, application of active control method such as microblowing effect in the incompressible, zero pressure gradient turbulent boundary layer was investigated. A series of experiments have been performed in two different wind tunnel facilities. Wind tunnel from Department of Aerodynamics and Fluid Mechanics (LAS) was used for the measurements for moderate Reynolds number range in co-operation with the wind tunnel from Laboratoire de M ́ecanique de Feiret Lille for large Reynolds number range. Measurements are conducted with the help of state-of-the-art techniques such as Laser Doppler Anemometry, Particle Image Velocimetry and electronic pressure sensors.
Preliminary Experimental Investigation of Effect of Free-stream Turbulence on Turbulent Boundary-layer Growth
Author: S. J. Kline
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 70
Book Description
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 70
Book Description
Experimental Investigation of the Turbulent Boundary Layer at High Reynolds Numbers and a Mach Number of 0.8
Author: L. Gaudet
Publisher:
ISBN:
Category :
Languages : en
Pages : 47
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 47
Book Description
Experimental Investigation of the Near Wall Flow Structure of a Low Reynolds Number 3-D Turbulent Boundary Layer
Author: J. L. Fleming
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Flow at Ultra-High Reynolds and Rayleigh Numbers
Author: Russell J. Donnelly
Publisher: Springer Science & Business Media
ISBN: 1461222303
Category : Science
Languages : en
Pages : 483
Book Description
Scientists have learned to use liquid and gaseous helium to overcome the limitations imposed by the usual wind and water tunnels for testing the performance of aircraft or the behavior of the atmosphere. This book covers fundamental studies of the turbulence problem, practical applications of turbulence, superfluid turbulence, cryogenic turbulence research, and new types of miniature flow instrumentation, all which are crucial for high Reynolds number research. This state-of-the-art presentation will interest physicists in fluid dynamics, engineers working with turbulent flows, and naval and aerospace engineers testing realistic parameter ranges.
Publisher: Springer Science & Business Media
ISBN: 1461222303
Category : Science
Languages : en
Pages : 483
Book Description
Scientists have learned to use liquid and gaseous helium to overcome the limitations imposed by the usual wind and water tunnels for testing the performance of aircraft or the behavior of the atmosphere. This book covers fundamental studies of the turbulence problem, practical applications of turbulence, superfluid turbulence, cryogenic turbulence research, and new types of miniature flow instrumentation, all which are crucial for high Reynolds number research. This state-of-the-art presentation will interest physicists in fluid dynamics, engineers working with turbulent flows, and naval and aerospace engineers testing realistic parameter ranges.
ASME 69-APMW-26
Author: Tony Maxworthy
Publisher:
ISBN:
Category : Laminar flow
Languages : en
Pages : 10
Book Description
Publisher:
ISBN:
Category : Laminar flow
Languages : en
Pages : 10
Book Description
Experimental Investigation of the Compressible Turbulent Boundary Layer at Very High Reynolds Numbers, M
Author: D. R. Moore
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description