Author: Daniel J. Dorney
Publisher:
ISBN:
Category :
Languages : en
Pages : 13
Book Description
Experimental and Numerical Investigation of Losses in Low-pressure Turbine Blade Rows
Author: Daniel J. Dorney
Publisher:
ISBN:
Category :
Languages : en
Pages : 13
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 13
Book Description
Experimental and Numerical Investigation of Losses in Low-Pressure Turbine Blade Rows
Author: Daniel J. Dorney
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
Book Description
Numerical Investigation of Low-pressure Turbine Blade Separation Control
Author: D. Postl
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
An Experimental Investigation of the Aerodynamic Losses for an Incident Tolerant Low Pressure Turbine Blade Over Moderate to Low Reynolds Numbers at Engine Representative Mach Numbers
Author: Jonathan Adam Long
Publisher:
ISBN: 9781321536645
Category : Electronic dissertations
Languages : en
Pages : 366
Book Description
Publisher:
ISBN: 9781321536645
Category : Electronic dissertations
Languages : en
Pages : 366
Book Description
Experimental Investigation of Loss in an Annular Cascade of Turbine-nozzle Blades of Free Vortex Design
Author: Hubert W. Allen
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 42
Book Description
An investigation of the flow pattern immediately downstream of an annular cascade of nozzle blades designed for vortex-type velocity distribution and hub discharge angle of approximately 65 degrees from axial was conducted in order to obtain a better understanding of the processes by which the distribution of losses and deviations from design turning angle occur. For the two Mach numbers investigated, the loass region at the outer shroud decreased while that at the inner shroud increased with increasing Mach number.
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 42
Book Description
An investigation of the flow pattern immediately downstream of an annular cascade of nozzle blades designed for vortex-type velocity distribution and hub discharge angle of approximately 65 degrees from axial was conducted in order to obtain a better understanding of the processes by which the distribution of losses and deviations from design turning angle occur. For the two Mach numbers investigated, the loass region at the outer shroud decreased while that at the inner shroud increased with increasing Mach number.
Impingement Jet Cooling in Gas Turbines
Author: R.S. Amano
Publisher: WIT Press
ISBN: 1845649060
Category : Science
Languages : en
Pages : 253
Book Description
Due to the requirement for enhanced cooling technologies on modern gas turbine engines, advanced research and development has had to take place in field of thermal engineering. Among the gas turbine cooling technologies, impingement jet cooling is one of the most effective in terms of cooling effectiveness, manufacturability and cost. The chapters contained in this book describe research on state-of-the-art and advanced cooling technologies that have been developed, or that are being researched, with a variety of approaches from theoretical, experimental, and CFD studies. The authors of the chapters have been selected from some of the most active researchers and scientists on the subject. This is the first to book published on the topics of gas turbines and heat transfer to focus on impingement cooling alone.
Publisher: WIT Press
ISBN: 1845649060
Category : Science
Languages : en
Pages : 253
Book Description
Due to the requirement for enhanced cooling technologies on modern gas turbine engines, advanced research and development has had to take place in field of thermal engineering. Among the gas turbine cooling technologies, impingement jet cooling is one of the most effective in terms of cooling effectiveness, manufacturability and cost. The chapters contained in this book describe research on state-of-the-art and advanced cooling technologies that have been developed, or that are being researched, with a variety of approaches from theoretical, experimental, and CFD studies. The authors of the chapters have been selected from some of the most active researchers and scientists on the subject. This is the first to book published on the topics of gas turbines and heat transfer to focus on impingement cooling alone.
Numerical Investigation of a Low Reynolds Number Flow Field in a Turbine Blade Row
Author: Shunji Enomoto
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Low Reynolds Number
Author: Mustafa Serdar Genç
Publisher: BoD – Books on Demand
ISBN: 9535104926
Category : Science
Languages : en
Pages : 176
Book Description
This book reports the latest development and trends in the low Re number aerodynamics, transition from laminar to turbulence, unsteady low Reynolds number flows, experimental studies, numerical transition modelling, control of low Re number flows, and MAV wing aerodynamics. The contributors to each chapter are fluid mechanics and aerodynamics scientists and engineers with strong expertise in their respective fields. As a whole, the studies presented here reveal important new directions toward the realization of applications of MAV and wind turbine blades.
Publisher: BoD – Books on Demand
ISBN: 9535104926
Category : Science
Languages : en
Pages : 176
Book Description
This book reports the latest development and trends in the low Re number aerodynamics, transition from laminar to turbulence, unsteady low Reynolds number flows, experimental studies, numerical transition modelling, control of low Re number flows, and MAV wing aerodynamics. The contributors to each chapter are fluid mechanics and aerodynamics scientists and engineers with strong expertise in their respective fields. As a whole, the studies presented here reveal important new directions toward the realization of applications of MAV and wind turbine blades.
Paper
Author:
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 506
Book Description
Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 506
Book Description
Proceedings of the ASME Turbo Expo 2002
Author:
Publisher:
ISBN:
Category : Aircraft gas-turbines
Languages : en
Pages : 594
Book Description
Publisher:
ISBN:
Category : Aircraft gas-turbines
Languages : en
Pages : 594
Book Description