Author: Robert S. Peterson
Publisher:
ISBN:
Category :
Languages : en
Pages : 246
Book Description
The report covers experimental work performed to determine the effect of nozzle divergence angle, specific heat ratio and plug nozzle configuration on turbine nozzle performance. Off design performance was the primary area of investigation. The effect of nozzle divergence angle was investigated with conical and contoured nozzles for two Mach numbers over a range of speed and pressure ratios. The performance of selected plug nozzle geometries was neasured over a range of speed and pressure ratios. The influence on performance of the gas specific heat ratios was experimentally determined by testing the same nozzle with gases of different specific heat ratios. The reduced experimental data is presented in tabular form as well as graphic presentation in several formats. (Author).
An Experimental Study of Nozzles and Specific Heat Ratio Effects on Off-Design Performance of Partial Admission Turbines
Author: Robert S. Peterson
Publisher:
ISBN:
Category :
Languages : en
Pages : 246
Book Description
The report covers experimental work performed to determine the effect of nozzle divergence angle, specific heat ratio and plug nozzle configuration on turbine nozzle performance. Off design performance was the primary area of investigation. The effect of nozzle divergence angle was investigated with conical and contoured nozzles for two Mach numbers over a range of speed and pressure ratios. The performance of selected plug nozzle geometries was neasured over a range of speed and pressure ratios. The influence on performance of the gas specific heat ratios was experimentally determined by testing the same nozzle with gases of different specific heat ratios. The reduced experimental data is presented in tabular form as well as graphic presentation in several formats. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 246
Book Description
The report covers experimental work performed to determine the effect of nozzle divergence angle, specific heat ratio and plug nozzle configuration on turbine nozzle performance. Off design performance was the primary area of investigation. The effect of nozzle divergence angle was investigated with conical and contoured nozzles for two Mach numbers over a range of speed and pressure ratios. The performance of selected plug nozzle geometries was neasured over a range of speed and pressure ratios. The influence on performance of the gas specific heat ratios was experimentally determined by testing the same nozzle with gases of different specific heat ratios. The reduced experimental data is presented in tabular form as well as graphic presentation in several formats. (Author).
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 268
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 268
Book Description
Turbine Technology
Author:
Publisher:
ISBN:
Category : Automobiles, Gas-turbine
Languages : en
Pages : 554
Book Description
Publisher:
ISBN:
Category : Automobiles, Gas-turbine
Languages : en
Pages : 554
Book Description
Heat Bibliography
Author:
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 452
Book Description
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 452
Book Description
Government Reports Announcements
Author:
Publisher:
ISBN:
Category : Technology
Languages : en
Pages : 1692
Book Description
Publisher:
ISBN:
Category : Technology
Languages : en
Pages : 1692
Book Description
Proceedings of the ... Intersociety Energy Conversion Engineering Conference
Author:
Publisher:
ISBN:
Category : Direct energy conversion
Languages : en
Pages : 1196
Book Description
Publisher:
ISBN:
Category : Direct energy conversion
Languages : en
Pages : 1196
Book Description
Government Reports Announcements & Index
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1430
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1430
Book Description
Government Reports Index
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 916
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 916
Book Description
Energy Research Abstracts
Author:
Publisher:
ISBN:
Category : Power resources
Languages : en
Pages : 982
Book Description
Publisher:
ISBN:
Category : Power resources
Languages : en
Pages : 982
Book Description
Turbine Aerodynamics
Author: Ronald H. Aungier
Publisher: American Society of Mechanical Engineers
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 424
Book Description
This book provides a thorough description of actual, working aerodynamic design and analysis systems, for both axial-flow and radial-flow turbines. It describes the basic fluid dynamic and thermodynamic principles, empirical models and numerical methods used for the full range of procedures and analytical tools that an engineer needs for virtually any type of aerodynamic design or analysis activity for both types of turbine. The book includes sufficient detail for readers to implement all or part of the systems. The author provides practical and effective design strategies for applying both turbine types, which are illustrated by design examples. Comparisons with experimental results are included to demonstrate the prediction accuracy to be expected. This book is intended for practicing engineers concerned with the design and development of turbines and related machinery.
Publisher: American Society of Mechanical Engineers
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 424
Book Description
This book provides a thorough description of actual, working aerodynamic design and analysis systems, for both axial-flow and radial-flow turbines. It describes the basic fluid dynamic and thermodynamic principles, empirical models and numerical methods used for the full range of procedures and analytical tools that an engineer needs for virtually any type of aerodynamic design or analysis activity for both types of turbine. The book includes sufficient detail for readers to implement all or part of the systems. The author provides practical and effective design strategies for applying both turbine types, which are illustrated by design examples. Comparisons with experimental results are included to demonstrate the prediction accuracy to be expected. This book is intended for practicing engineers concerned with the design and development of turbines and related machinery.