Design and Performance of Gas Turbine Power Plants 1st Edition by William Hawthorne, Walter Olson ISBN 978-0691626154 0691626154
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Product details:
ISBN 10: 0691626154
ISBN 13: 978-0691626154
Author: William R. Hawthorne, Walter T. Olson
Volume XI of the High Speed Aerodynamics and Jet Propulsion series. Edited by W.R. Hawthorne and W.T. Olson. This is a comprehensive presentation of basic problems involved in the design of aircraft gas turbines, including sections covering requirements and processes, experimental techniques, fuel injection, flame stabilization, mixing processes, fuels, combustion chamber development, materials for gas turbine applications, turbine blade vibration, and performance.
Originally published in 1960.
The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Table of contents:
PART 1. INTRODUCTION
A. General Considerations
William R. Hawthorne, Engineering Laboratory, Cambridge University, Cambridge, England
1. Combustion Chamber Design
2. Problems of Materials and Mechanical Strength
3. Performance
PART 2. COMBUSTION CHAMBER DESIGN
B. Requirements and Processes
Peter Lloyd, National Gas Turbine Establishment, Farn-borough, Hampshire, England
1. Basic Requirements
2. Techniques
3. Processes
4. Performance of the Complete Combustion System
5. Cited References
C. Experimental Techniques
Hoyt C. Hottel and Glenn C. Williams, Department of Chemical Engineering, Massachusetts Institute of Tech-nology, Cambridge, Massachusetts
1. General Discussion
2. Temperature Measurements
3. Pressure Measurements
4. Velocity Measurements
5. Mass Velocity Measurements
6. Measurements of Gas Composition
7. Traverse Measurements
8. Measurement of Time-Dependent Properties
9. Cited References
D. Fuel Injection
Alec Radcliffe, Applied Physics Laboratory, The Johns Hop-kins University, Silver Spring, Maryland
1. Introduction
Activate
2. Liquid Injection through Simple Holes
3. Flat Sprays
4. Swirl Atomizers
5. Air Blast Atomization
6. Disk or Cup Atomizers
7. Vaporization
8. Gaseous Injection
9. Solid Fuels
10. Cited References and Bibliography
E. Flame Stabilization
J. Howard Childs, Lewis Flight Propulsion Laboratory, National Aeronautics and Space Administration, Cleveland, Ohio
Chapter 1. Flame Stabilization by Bluff Bodies in Gaseous Fuel-Air Mixtures
1. Introduction
2. Flow about Bluff Bodies
3. Effect of Flow and System Variables on Flame Stabilization
4. Theories of Flame Stabilization
Chapter 2. Flame Stabilization by Bluff Bodies in Air-Fuel Spray Mixtures
5. Introduction
6. Mechanism of Flame Stabilization
7. Effect of Fuel Atomization and Fuel Volatility
8. Effect of Flame Holder Size and Shape
Chapter 3. Flame Stabilization inside Perforated Liners
9. Introduction
10. Effect of Flow and Design Variables on Flame Stabilization
11. Theory of Flame Stabilization
12. Possible Relation between Combustion Efficiency and Flame Stability
Chapter 4. Flame Stabilization in Boundary Layers
13. Characteristics of Bunsen Flames
14. Mechanism of Flame Stabilization
15. Cited References
F. Mixing Processes
Charles C. Graves, Nuclear Development Corporation of America, White Plains, New York
Wilfred E. Scull, Lewis Flight Propulsion Laboratory, Na-tional Aeronautics and Space Administration, Cleveland, Ohio
2. Mixing Theory for simple Jet Systems
3. Experiments on Mixing and Penetration in Simple Jet Systems
4. Mixing of Gases with Burning
5. Liquid-Air Mixing
6. Mixing in Combustion Chambers
7. Cited References
G. Fuels for Aircraft Gas Turbine Engines
Louis C. Gibbons, The Ohio Oil Company, Littleton, Colorado
1. Introduction
2. Fuel Performance in Engines
3. Fuel Behavior in Aircraft Fuel Systems
4. Fuel Specifications and Availability
5. Concluding Remarks
6. Cited References
H. Combustion Chamber Development
Walter T. Olson, Lewis Flight Propulsion Laboratory, National Aeronautics and Space Administration, Cleveland, Ohio
1. Introduction
2. Historical Development
3. Combustor Performance
4. Combustor Arrangement
5. Combustor Size
6. Primary Zone
7. Secondary Zone
8. Construction and Durability
9. Future Trends for Design
10. Cited References
PART 3. MECHANICAL AND METALLURGICAL ASPECTS
I. Mechanics of Materials for Gas Turbine Applications
Egon Orowan, Department of Mechanical Engineering, Massachusetts Institute of Technology, Cambridge, Mas-sachusetts
C. Richard Soderberg, School of Engineering, Massachusetts Institute of Technology, Cambridge, Massachusett
1. Introduction
2. Influence of Temperature on Mechanical Behavior of Metals and Other Crystalline Materials. General Survey
3. Yield Stress. Dislocations and Plastic Deformation
4. Strain Hardening
5. Precipitation Hardening
6. Transient Creep (Cold Creep)
7. Viscous Creep (Hot Creep)
8. Creep Fracture
9. Creep in Engineering Design
10. Creep Tests and Their Evaluation
11. Design for Temperature Rise during Service
12. Plastic Instability; Ultimate Strength. Instability of Non-Newtonian Viscous Materials
13. Plastic Deformation and Creep under Triaxial Stress
14. Fatigue
15. Materials for High Temperature Service
16. Cited References
J. Flutter Problems in Gas Turbines
Jan R. Schnittger, Gas Turbine Department, Svenska Tur-binfabriks Aktiebolaget Ljungström, Finspong, Sweden
1. Introduction
2. Equations of Motion for Equivalent Airfoil
3. Aerodynamic Forces in Potential Flow
4. Forced Vibrations of Two-Dimensional Airfoils in Potential Flow
5. Aerodynamic Forces in Stalled Flow
6. The Stress Problem of Vibrating Compressor Blades
7. Cited References and Bibliography
PART 4. TURBINE POWER PLANTS
K. Performance
Dennis H. Mallinson and Sidney J. Moyes, National Gas Turbine Establishment, Farnborough, Hampshire, England
1. Basic Constant Pressure Gas Turbine Cycle
2. Basic Thermodynamics of the Aircraft Turbine Engine Cycle
3. Nondimensional Representation of Compressor and Tur-bine Performance
4. Determination of Equilibrium Running Conditions by Matching of Component Characteristics
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5. Performance of Simple Jet and Propeller Turbine Engines
6. Equilibrium Running of More Complex Engines
7. Cited References and Bibliography
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Tags: William Hawthorne, Walter Olson, Design and Performance, Turbine Power