Author:
Publisher:
ISBN:
Category :
Languages : ja
Pages : 15
Book Description
Analysis of two-dimensional turbine cascade flow by finite area method
Author:
Publisher:
ISBN:
Category :
Languages : ja
Pages : 15
Book Description
Publisher:
ISBN:
Category :
Languages : ja
Pages : 15
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704
Book Description
Two-dimensional Rotating Cascade Flow Analysis Using a Control Volume Finite Element Method [microform]
Author: Mark Hodgson
Publisher: National Library of Canada
ISBN: 9780315329423
Category :
Languages : en
Pages : 229
Book Description
Publisher: National Library of Canada
ISBN: 9780315329423
Category :
Languages : en
Pages : 229
Book Description
Computational Fluid Dynamics Review 1998 (In 2 Volumes)
Author: Mohamed M Hafez
Publisher: World Scientific
ISBN: 9814495778
Category : Science
Languages : en
Pages : 1169
Book Description
The first volume of CFD Review was published in 1995. The purpose of this new publication is to present comprehensive surveys and review articles which provide up-to-date information about recent progress in computational fluid dynamics, on a regular basis. Because of the multidisciplinary nature of CFD, it is difficult to cope with all the important developments in related areas. There are at least ten regular international conferences dealing with different aspects of CFD.It is a real challenge to keep up with all these activities and to be aware of essential and fundamental contributions in these areas. It is hoped that CFD Review will help in this regard by covering the state-of-the-art in this field.The present book contains sixty-two articles written by authors from the US, Europe, Japan and China, covering the main aspects of CFD. There are five sections: general topics, numerical methods, flow physics, interdisciplinary applications, parallel computation and flow visualization. The section on numerical methods includes grids, schemes and solvers, while that on flow physics includes incompressible and compressible flows, hypersonics and gas kinetics as well as transition and turbulence. This book should be useful to all researchers in this fast-developing field.
Publisher: World Scientific
ISBN: 9814495778
Category : Science
Languages : en
Pages : 1169
Book Description
The first volume of CFD Review was published in 1995. The purpose of this new publication is to present comprehensive surveys and review articles which provide up-to-date information about recent progress in computational fluid dynamics, on a regular basis. Because of the multidisciplinary nature of CFD, it is difficult to cope with all the important developments in related areas. There are at least ten regular international conferences dealing with different aspects of CFD.It is a real challenge to keep up with all these activities and to be aware of essential and fundamental contributions in these areas. It is hoped that CFD Review will help in this regard by covering the state-of-the-art in this field.The present book contains sixty-two articles written by authors from the US, Europe, Japan and China, covering the main aspects of CFD. There are five sections: general topics, numerical methods, flow physics, interdisciplinary applications, parallel computation and flow visualization. The section on numerical methods includes grids, schemes and solvers, while that on flow physics includes incompressible and compressible flows, hypersonics and gas kinetics as well as transition and turbulence. This book should be useful to all researchers in this fast-developing field.
Aerothermodynamics of Aircraft Engine Components
Author: Gordon C. Oates
Publisher: AIAA
ISBN: 9781600860058
Category : Aerothermodynamics
Languages : en
Pages : 568
Book Description
Annotation Design and R & D engineers and students will value the comprehensive, meticulous coverage in this volume. Beginning with the basic principles and concepts of aeropropulsion combustion, chapters explore specific processes, limitations, and analytical methods as they bear on component design.
Publisher: AIAA
ISBN: 9781600860058
Category : Aerothermodynamics
Languages : en
Pages : 568
Book Description
Annotation Design and R & D engineers and students will value the comprehensive, meticulous coverage in this volume. Beginning with the basic principles and concepts of aeropropulsion combustion, chapters explore specific processes, limitations, and analytical methods as they bear on component design.
Applied Mechanics Reviews
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 960
Book Description
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 960
Book Description
Journal of Engineering for Power
Author:
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 976
Book Description
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 976
Book Description
Japanese Science and Technology
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 724
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 724
Book Description
An Analytical Study of Flow Losses Through a Two-Dimensional Turbine Cascade with Boundary Layer Injection
Author: W. Tabakoff
Publisher:
ISBN:
Category : Cascades (Fluid dynamics)
Languages : en
Pages : 52
Book Description
A method for determining the performance of a two-dimensional turbine cascade with boundary layer injection is developed using existing incompressible boundary layer approximate solutions with a new formulation for the injection. The overall cascade loss includes friction and wake mixing losses. The results of the analysis are compared with experimentally obtained data as a check of the validity of the new analytical method. (Author).
Publisher:
ISBN:
Category : Cascades (Fluid dynamics)
Languages : en
Pages : 52
Book Description
A method for determining the performance of a two-dimensional turbine cascade with boundary layer injection is developed using existing incompressible boundary layer approximate solutions with a new formulation for the injection. The overall cascade loss includes friction and wake mixing losses. The results of the analysis are compared with experimentally obtained data as a check of the validity of the new analytical method. (Author).
Aeronautical Engineering
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580
Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580
Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)