Author: Constantine John Strataridakis
Publisher:
ISBN:
Category :
Languages : en
Pages : 358
Book Description
Hot-wire Anemometry Measurements of Turbulent Boundary Later Flow Past a Two-dimensional Obstacle
Author: Constantine John Strataridakis
Publisher:
ISBN:
Category :
Languages : en
Pages : 358
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 358
Book Description
Hot-wire Anemometry Measurement of the Turbulent Boundary Layer at Low Reynolds Numbers
Measurements of the Transverse Velocity of a Separating Turbulent Boundary Layer
Author: Klara Shiloh
Publisher:
ISBN:
Category :
Languages : en
Pages : 80
Book Description
The problem of turbulent boundary layer separation due to an adverse pressure gradient is an old but still important problem in many fluid flow devices. Until recent years little quantitative experimental information was available on the flow structure downstream of separation because of the lack of proper instrumentation. The directionally-sensitive laser anemometer now provides the ability to accurately measure the instantaneous flow direction and magnitude. Simpson, Chew, and Shivaprasad (1980) presented a number of experimental results for a nominally two-dimensional separating turbulent boundary layer for an airfoil-type flow in which the flow was accelerated and then decelerated until separation. Upstream of separation single and cross-wire hot-wire anemometer measurements were also presented. In addition to confirming the earlier conclusions of Simpson et al. (1977), these results provided new insights about the separated flow region. From that work, the backflow appears to be supplied by the large eddy structure rather than coming from far downstream. It also was suggested that downstream of fully-developed separation the mean backflow could be divided into three layers: a viscous layer nearest the wall that is dominated by the turbulent flow unsteadiness but with little Reynolds shearing stress effects; a rather uniform mean velocity intermediate layer that seems to act as an overlap region between the viscous wall and outer regions; and the outer backflow region that is really part of the large-scaled outer region. The results presented here support the earlier flow model of Simpson et al. (1980).
Publisher:
ISBN:
Category :
Languages : en
Pages : 80
Book Description
The problem of turbulent boundary layer separation due to an adverse pressure gradient is an old but still important problem in many fluid flow devices. Until recent years little quantitative experimental information was available on the flow structure downstream of separation because of the lack of proper instrumentation. The directionally-sensitive laser anemometer now provides the ability to accurately measure the instantaneous flow direction and magnitude. Simpson, Chew, and Shivaprasad (1980) presented a number of experimental results for a nominally two-dimensional separating turbulent boundary layer for an airfoil-type flow in which the flow was accelerated and then decelerated until separation. Upstream of separation single and cross-wire hot-wire anemometer measurements were also presented. In addition to confirming the earlier conclusions of Simpson et al. (1977), these results provided new insights about the separated flow region. From that work, the backflow appears to be supplied by the large eddy structure rather than coming from far downstream. It also was suggested that downstream of fully-developed separation the mean backflow could be divided into three layers: a viscous layer nearest the wall that is dominated by the turbulent flow unsteadiness but with little Reynolds shearing stress effects; a rather uniform mean velocity intermediate layer that seems to act as an overlap region between the viscous wall and outer regions; and the outer backflow region that is really part of the large-scaled outer region. The results presented here support the earlier flow model of Simpson et al. (1980).
Scientific and Technical Aerospace Reports
Energy Research Abstracts
Wall Neighbourhood Measurements in Turbulent Boundary Layers Using a Hot Wire Anemometer
Proceedings
Author: Jack E. Cermak
Publisher:
ISBN:
Category : Wind power
Languages : en
Pages : 556
Book Description
Publisher:
ISBN:
Category : Wind power
Languages : en
Pages : 556
Book Description
Applied Mechanics Reviews
Thermal Measurements in Electronics Cooling
Author: Kaveh Azar
Publisher: CRC Press
ISBN: 1000102769
Category : Technology & Engineering
Languages : en
Pages : 496
Book Description
Filled with careful explanations, step-by-step instructions, and useful examples, this handbook focuses on real-world considerations and applications of thermal measurement methods in electronics cooling. Fifteen experts in thermal engineering combine their expertise to create a complete guide to this complex topic. This practical reference covers all aspects of thermal characterization in electronics cooling and thermal management. The first part of the book introduces the concept of electronics cooling and its associated thermal phenomenon and explains why experimental investigation is required. Subsequent chapters explain methods of measuring different parameters and introduce relevant examples. Sources for locating needed equipment, tables, checklists, and to-do lists are included. Sample calculations and methodologies for error analysis ensure that you can put this valuable information to use in your work.
Publisher: CRC Press
ISBN: 1000102769
Category : Technology & Engineering
Languages : en
Pages : 496
Book Description
Filled with careful explanations, step-by-step instructions, and useful examples, this handbook focuses on real-world considerations and applications of thermal measurement methods in electronics cooling. Fifteen experts in thermal engineering combine their expertise to create a complete guide to this complex topic. This practical reference covers all aspects of thermal characterization in electronics cooling and thermal management. The first part of the book introduces the concept of electronics cooling and its associated thermal phenomenon and explains why experimental investigation is required. Subsequent chapters explain methods of measuring different parameters and introduce relevant examples. Sources for locating needed equipment, tables, checklists, and to-do lists are included. Sample calculations and methodologies for error analysis ensure that you can put this valuable information to use in your work.
Velocity, Intermittency, and Turbulence Intensity Measurements in the Boundary Layer of an Accelerated Flow
Author: Donald R. Boldman
Publisher:
ISBN:
Category : Anemometer
Languages : en
Pages : 44
Book Description
Hot-wire anemometer for velocity, intermittancy, and turbulence intensity measurements in boundary layer of accelerated flow.
Publisher:
ISBN:
Category : Anemometer
Languages : en
Pages : 44
Book Description
Hot-wire anemometer for velocity, intermittancy, and turbulence intensity measurements in boundary layer of accelerated flow.