Author: Thomas Charles Adamson
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 724
Book Description
Transonic Flow Problems in Turbomachinery
Author: Thomas Charles Adamson
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 724
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 724
Book Description
Transonic Flows in Axial Turbomachinery
Transonic Flows in Axial Turbomachinery
Transonic Flows in Axial Turbomachinery, February 2-6, 1976
Author: Von Karman Institute for Fluid Dynamics
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Transonic Flow Analysis in Axial-flow Turbomachinery Cascades by the Time-dependent Method of Characteristics
Author: Robert Anthony Delaney
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 210
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 210
Book Description
Aerodynamic Behavior of Axial Flow Turbomachinery Operating in Transient Transonic Flow Regimes
Author: Gregory Scott Heinlein
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 161
Book Description
The purpose of the current work is to study the transient behavior of axial flow turbomachines in transonic environments. The first part is focused on the aerodynamic behavior of a coupled boundary layer ingesting inlet – distortion tolerant fan for use in next generation aircraft. The second part is focused on stall detection in transonic compressors. The reason these two are covered is that the fan and compressor of this future system would be mechanically linked. The fan behaves dynamically in the presence of a distortion and exhibits non-uniform flow downstream of the fan. An engine core, comprised of compressor stages, would have to operate in that distorted flow possibly inducing stall. Therefore, understanding the behavior of the fan and developing advanced stall detection methods are important for the successful implementation of these future systems.
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 161
Book Description
The purpose of the current work is to study the transient behavior of axial flow turbomachines in transonic environments. The first part is focused on the aerodynamic behavior of a coupled boundary layer ingesting inlet – distortion tolerant fan for use in next generation aircraft. The second part is focused on stall detection in transonic compressors. The reason these two are covered is that the fan and compressor of this future system would be mechanically linked. The fan behaves dynamically in the presence of a distortion and exhibits non-uniform flow downstream of the fan. An engine core, comprised of compressor stages, would have to operate in that distorted flow possibly inducing stall. Therefore, understanding the behavior of the fan and developing advanced stall detection methods are important for the successful implementation of these future systems.
Transonic Blade-to-Blade Flows in Axial Turbomachinery
Author: Von Karman Institute for Fluid Dynamics
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Axial Turbine Aerodynamics for Aero-engines
Author: Zhengping Zou
Publisher: Springer
ISBN: 9811057508
Category : Technology & Engineering
Languages : en
Pages : 572
Book Description
This book is a monograph on aerodynamics of aero-engine gas turbines focusing on the new progresses on flow mechanism and design methods in the recent 20 years. Starting with basic principles in aerodynamics and thermodynamics, this book systematically expounds the recent research on mechanisms of flows in axial gas turbines, including high pressure and low pressure turbines, inter-turbine ducts and turbine rear frame ducts, and introduces the classical and innovative numerical evaluation methods in different dimensions. This book also summarizes the latest research achievements in the field of gas turbine aerodynamic design and flow control, and the multidisciplinary conjugate problems involved with gas turbines. This book should be helpful for scientific and technical staffs, college teachers, graduate students, and senior college students, who are involved in research and design of gas turbines.
Publisher: Springer
ISBN: 9811057508
Category : Technology & Engineering
Languages : en
Pages : 572
Book Description
This book is a monograph on aerodynamics of aero-engine gas turbines focusing on the new progresses on flow mechanism and design methods in the recent 20 years. Starting with basic principles in aerodynamics and thermodynamics, this book systematically expounds the recent research on mechanisms of flows in axial gas turbines, including high pressure and low pressure turbines, inter-turbine ducts and turbine rear frame ducts, and introduces the classical and innovative numerical evaluation methods in different dimensions. This book also summarizes the latest research achievements in the field of gas turbine aerodynamic design and flow control, and the multidisciplinary conjugate problems involved with gas turbines. This book should be helpful for scientific and technical staffs, college teachers, graduate students, and senior college students, who are involved in research and design of gas turbines.
Computational Methods in Turbomachinery
Author: Institution of Mechanical Engineers (Great Britain). Power Industries Division
Publisher:
ISBN:
Category : Thermodynamics
Languages : en
Pages : 294
Book Description
Publisher:
ISBN:
Category : Thermodynamics
Languages : en
Pages : 294
Book Description
Unsteady Phenomena in Turbomachinery
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580
Book Description