Author: Leslie Gary Leal
Publisher:
ISBN:
Category : Fluid flow
Languages : en
Pages : 446
Book Description
A Study of Steady, Closed Streamline Flows at Large Reynolds Number
Author: Leslie Gary Leal
Publisher:
ISBN:
Category : Fluid flow
Languages : en
Pages : 446
Book Description
Publisher:
ISBN:
Category : Fluid flow
Languages : en
Pages : 446
Book Description
Long and Slender Closed Streamline Flows at Large Reynolds Numbers
Author: Mark Louis Schrader
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 444
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 444
Book Description
An Investigation Into the Nature of Steady Separated Flows at Large Reynolds Numbers
Author: Andrew S. Grove
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 336
Book Description
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 336
Book Description
Mathematical Theory of Steady Compressible Swirl Flows with Closed Streamlines at High Reynolds Numbers
Author: Karl G. Guderley
Publisher:
ISBN:
Category : Inviscid flow
Languages : en
Pages : 280
Book Description
The paper presents a theory of axi-symmetric steady compressible swirl flows in which the stream lines are closed, under the assumption that the Reynolds number is large. In principle the flow field is determined by the equations for an inviscid flow; but, if the stream lines are closed, additional conditions arise which are primarily determined by the dissipative terms. They arise by purely mathematical arguments as the solvability conditions for the approximation of the next order in a development with respect to the reciprocal of the Reynolds number. These conditions can be interpreted in physical terms. Various transformations are carried out, to prepare the equations for numerical work. The mathematical structure of the operators occurring in the solvability conditions and its relation to the parameters which are suggested by physical considerations is studied in detail. The solution for the potential vortex is compatible with this approach only if the viscosity coefficient is constant with the Prandtl number is 1/2. (Author).
Publisher:
ISBN:
Category : Inviscid flow
Languages : en
Pages : 280
Book Description
The paper presents a theory of axi-symmetric steady compressible swirl flows in which the stream lines are closed, under the assumption that the Reynolds number is large. In principle the flow field is determined by the equations for an inviscid flow; but, if the stream lines are closed, additional conditions arise which are primarily determined by the dissipative terms. They arise by purely mathematical arguments as the solvability conditions for the approximation of the next order in a development with respect to the reciprocal of the Reynolds number. These conditions can be interpreted in physical terms. Various transformations are carried out, to prepare the equations for numerical work. The mathematical structure of the operators occurring in the solvability conditions and its relation to the parameters which are suggested by physical considerations is studied in detail. The solution for the potential vortex is compatible with this approach only if the viscosity coefficient is constant with the Prandtl number is 1/2. (Author).
Steady Flow Past Sudden Expansions at Large Reynolds Number
Scientific and Technical Aerospace Reports
On Closed Streamline Flows
Recent Developments in Theoretical and Experimental Fluid Mechanics
Author: U. Müller
Publisher: Springer Science & Business Media
ISBN: 3642672205
Category : Science
Languages : en
Pages : 663
Book Description
Dedicated to Prof. Dr.-Ing. J. Zierep
Publisher: Springer Science & Business Media
ISBN: 3642672205
Category : Science
Languages : en
Pages : 663
Book Description
Dedicated to Prof. Dr.-Ing. J. Zierep
Basic Aerodynamics
Author: Gary A. Flandro
Publisher: Cambridge University Press
ISBN: 1139498614
Category : Technology & Engineering
Languages : en
Pages : 433
Book Description
In the rapidly advancing field of flight aerodynamics, it is especially important for students to master the fundamentals. This text, written by renowned experts, clearly presents the basic concepts of underlying aerodynamic prediction methodology. These concepts are closely linked to physical principles so that they are more readily retained and their limits of applicability are fully appreciated. Ultimately, this will provide students with the necessary tools to confidently approach and solve practical flight vehicle design problems of current and future interest. This book is designed for use in courses on aerodynamics at an advanced undergraduate or graduate level. A comprehensive set of exercise problems is included at the end of each chapter.
Publisher: Cambridge University Press
ISBN: 1139498614
Category : Technology & Engineering
Languages : en
Pages : 433
Book Description
In the rapidly advancing field of flight aerodynamics, it is especially important for students to master the fundamentals. This text, written by renowned experts, clearly presents the basic concepts of underlying aerodynamic prediction methodology. These concepts are closely linked to physical principles so that they are more readily retained and their limits of applicability are fully appreciated. Ultimately, this will provide students with the necessary tools to confidently approach and solve practical flight vehicle design problems of current and future interest. This book is designed for use in courses on aerodynamics at an advanced undergraduate or graduate level. A comprehensive set of exercise problems is included at the end of each chapter.
Closed Streamline Flows Past Rotating Particles
Author: Gary Gordon Poe
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 310
Book Description
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 310
Book Description