Author: Rex Wayne Shumway
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 217
Book Description
Results for laminar gas flow in annuli with variation of fluid properties were obtained for both fully developed and uniform entry velocity profiles by solving the appropriate differential equations in finite difference form. The solutions are valid in flow situations where axial conduction may be neglected, and Mach number is low boundary layer assumptions apply and use of the perfect gas equation of state is defensible. All annuli computations were made with a radius ratio of 0.25, which differs sufficiently from the limiting cases of circular tubes and parallel plates to portray geometry well. Numerical results with full variation of the gas properties were obtained. A heating rate was chosen which would lead to peak wall-to-bulk temperature ratios of about three to five and, therefore, significant property gradients. Results are comparable to those found for circular tubes, except fully-established profiles with significant property variation could exist downstream if the unheated wall was held at a constant temperature. In the thermal entry, heat transfer parameters did not differ substantially from constant property predictions. The friction factors and, hence, pressure drop, did vary significantly. With uniform entering velocities these observations were further tempered by dominance of the usual effects of flow development. (Author).
Variable Properties Laminar Gas Flow Heat Transfer and Pressure Drop in Annuli
Author: Rex Wayne Shumway
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 217
Book Description
Results for laminar gas flow in annuli with variation of fluid properties were obtained for both fully developed and uniform entry velocity profiles by solving the appropriate differential equations in finite difference form. The solutions are valid in flow situations where axial conduction may be neglected, and Mach number is low boundary layer assumptions apply and use of the perfect gas equation of state is defensible. All annuli computations were made with a radius ratio of 0.25, which differs sufficiently from the limiting cases of circular tubes and parallel plates to portray geometry well. Numerical results with full variation of the gas properties were obtained. A heating rate was chosen which would lead to peak wall-to-bulk temperature ratios of about three to five and, therefore, significant property gradients. Results are comparable to those found for circular tubes, except fully-established profiles with significant property variation could exist downstream if the unheated wall was held at a constant temperature. In the thermal entry, heat transfer parameters did not differ substantially from constant property predictions. The friction factors and, hence, pressure drop, did vary significantly. With uniform entering velocities these observations were further tempered by dominance of the usual effects of flow development. (Author).
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 217
Book Description
Results for laminar gas flow in annuli with variation of fluid properties were obtained for both fully developed and uniform entry velocity profiles by solving the appropriate differential equations in finite difference form. The solutions are valid in flow situations where axial conduction may be neglected, and Mach number is low boundary layer assumptions apply and use of the perfect gas equation of state is defensible. All annuli computations were made with a radius ratio of 0.25, which differs sufficiently from the limiting cases of circular tubes and parallel plates to portray geometry well. Numerical results with full variation of the gas properties were obtained. A heating rate was chosen which would lead to peak wall-to-bulk temperature ratios of about three to five and, therefore, significant property gradients. Results are comparable to those found for circular tubes, except fully-established profiles with significant property variation could exist downstream if the unheated wall was held at a constant temperature. In the thermal entry, heat transfer parameters did not differ substantially from constant property predictions. The friction factors and, hence, pressure drop, did vary significantly. With uniform entering velocities these observations were further tempered by dominance of the usual effects of flow development. (Author).
Analytical and Experimental Study of Compressible Laminar-flow Heat Transfer and Pressure Drop of a Gas in a Uniformly Heated Tube
Author: Alden F. Presler
Publisher:
ISBN:
Category : Gas flow
Languages : en
Pages : 52
Book Description
Publisher:
ISBN:
Category : Gas flow
Languages : en
Pages : 52
Book Description
The Effect of Transverse Temperature Gradients on the Heat Transfer and Friction for Laminar Flow of Gases
Author: Monty E. Davenport
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 124
Book Description
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 124
Book Description
Analysis of Developing Laminar Flow and Heat Transfer in a Tube for a Gas with Cooling
Author: Alden F. Presler
Publisher:
ISBN:
Category : Cooling
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Cooling
Languages : en
Pages : 44
Book Description
Laminar Flow Forced Convection in Ducts
Author: R. K. Shah
Publisher: Academic Press
ISBN: 1483191303
Category : Technology & Engineering
Languages : en
Pages : 492
Book Description
Laminar Flow Forced Convection in Ducts is a sourcebook for compact heat exchanger analytical data. This book describes the analytical solutions for laminar fluid flow and forced convection heat transfer in circular and noncircular pipes, including applicable differential equations and boundary conditions involving velocity and temperature problems of fluid flow. The book also discusses fluid flow—how much power is required to pump fluids through the heat exchanger, as well as the heat transfer—the determination of q" distribution, and the temperature of fluid and walls. The text also analyzes the coolant or heat transfer fluid flows in a nuclear power reactor composed of a bundle of circular section fuel rods located inside a round tube. R.A. Axford addresses fluid flow and heat transfers results for the rod bundle geometry in "Heat Transfer in Rod Bundles." The book also provides an overview and guidelines that can be used for the designer and the applied mathematician. This book is suitable for engineers working in electronics, aerospace, instrumentation, and biomechanics that use cooling or heating exchanges or solar collection systems.
Publisher: Academic Press
ISBN: 1483191303
Category : Technology & Engineering
Languages : en
Pages : 492
Book Description
Laminar Flow Forced Convection in Ducts is a sourcebook for compact heat exchanger analytical data. This book describes the analytical solutions for laminar fluid flow and forced convection heat transfer in circular and noncircular pipes, including applicable differential equations and boundary conditions involving velocity and temperature problems of fluid flow. The book also discusses fluid flow—how much power is required to pump fluids through the heat exchanger, as well as the heat transfer—the determination of q" distribution, and the temperature of fluid and walls. The text also analyzes the coolant or heat transfer fluid flows in a nuclear power reactor composed of a bundle of circular section fuel rods located inside a round tube. R.A. Axford addresses fluid flow and heat transfers results for the rod bundle geometry in "Heat Transfer in Rod Bundles." The book also provides an overview and guidelines that can be used for the designer and the applied mathematician. This book is suitable for engineers working in electronics, aerospace, instrumentation, and biomechanics that use cooling or heating exchanges or solar collection systems.
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 666
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 666
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Research in Progress
Author:
Publisher:
ISBN:
Category : Military research
Languages : en
Pages : 834
Book Description
Publisher:
ISBN:
Category : Military research
Languages : en
Pages : 834
Book Description
Heat Transfer with Laminar Flow in Concentric Annuli with Constant and Arbitrary Variable Axial Wall Temperature
Author: R. Viskanta
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 54
Book Description
Results were generalized to apply to the situation of arbitrary longitudinal variation of the wall temperatures of the annulus. As an illustration of the method, an extension is explicitly given for a linear increase of all temperature with axial distance.
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 54
Book Description
Results were generalized to apply to the situation of arbitrary longitudinal variation of the wall temperatures of the annulus. As an illustration of the method, an extension is explicitly given for a linear increase of all temperature with axial distance.
Heat Transfer in Gas-Cooled Annular Channels
Author: Jurgis Vilemas
Publisher: Springer
ISBN:
Category : Science
Languages : en
Pages : 248
Book Description
Publisher: Springer
ISBN:
Category : Science
Languages : en
Pages : 248
Book Description
Fluid Mechanics and Heat Transfer for Gases (air, He, H2 and N2) Flowing Single Phase in Closed Channels
Author: Rose Kraft
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 40
Book Description
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 40
Book Description