Saeed Farokhi (USA University of Kansas)

Aircraft Propulsion

Cleaner, Leaner, and Greener

• Gebundenes Buch

Produktbeschreibung

AIRCRAFT PROPULSION

Produktdetails

• Verlag: Wiley / Wiley & Sons
• Artikelnr. des Verlages: 1W119718640
• 3. Aufl.
• Seitenzahl: 1040
• Erscheinungstermin: 14. September 2021
• Englisch
• Abmessung: 263mm x 190mm x 54mm
• Gewicht: 2124g
• ISBN-13: 9781119718642
• ISBN-10: 1119718643
• Artikelnr.: 60894455

Autorenporträt

Saeed Farokhi, PhD, is Professor Emeritus of Aerospace Engineering at the University of Kansas, USA. His main areas of research focus are propulsion systems, flow control, renewable energy, and computational fluid dynamics. He is Fellow of the Royal Aeronautical Society and the American Society of Mechanical Engineers. He is Associate Fellow of the American Institute of Aeronautics and Astronautics.

Inhaltsangabe

Preface to the Third Edition

Preface to the Second Edition

Preface to the First Edition

1. Introduction

1.1 History of the Airbreathing Jet Engine, a Twentieth-Century Invention--The Beginning

1.2 Innovations in Aircraft Gas Turbine Engines

1.2.1 Multispool Configuration

1.2.2 Variable Stator

1.2.3 Transonic Compressor

1.2.4 Low-Emission Combustor

1.2.5 Turbine Cooling

1.2.6 Exhaust Nozzles

1.2.7 Modern Materials and Manufacturing Techniques

1.3 Twenty-first Century Aviation Goal: Sustainability

1.3.1 Combustion Emissions

1.3.2 Greenhouse Gases

1.3.3 Fuels for Sustainable Aviation

1.4 New Engine Concepts in Sustainable Aviation

1.4.1 Advanced GT Concepts: ATP/CROR and GTF

1.4.2 Adaptive Cycle Engine

1.4.3 Advanced Airbreathing Rocket Technology

1.4.4 Wave Rotor Topping Cycle

1.4.5 Pulse Detonation Engine (PDE)

1.4.6 Millimeter-Scale Gas Turbine Engines: Triumph of MEMS and Digital Fabrication

1.4.7 Combined Cycle Propulsion: Engines from Takeoff to Space

1.4.8 Hybrid-Electric and Distributed Electric Propulsion

1.5 New Vehicle Technologies

1.6 Summary

1.7 Roadmap for the Third Edition

References

Problems

2. Compressible Flow with Heat and Friction: A Review

2.1 Introduction

2.2 A Brief Review of Thermodynamics

2.3 Isentropic Process and Isentropic Flow

2.4 Conservation Principles for Systems and Control Volumes

2.5 Speed of Sound & Mach Number

2.6 Stagnation State

2.7 Quasi-One-Dimensional Flow

2.8 Area-Mach Number Relationship

2.9 Sonic Throat

2.10 Waves in Supersonic Flow

2.11 Normal Shocks

2.12 Oblique Shocks

2.13 Conical Shocks

2.14 Expansion Waves

2.15 Frictionless, Constant-Area Duct Flow with Heat Transfer: Rayleigh Flow

2.16 Adiabatic Flow of a Calorically Perfect Gas in a Constant-Area Duct with Friction: Fanno Flow

2.17 Friction (Drag) Coefficient Cf and D'Arcy Friction Factor fD

2.18 Dimensionless Parameters

2.19 Fluid Impulse

2.20 Summary of Fluid Impulse

References

Problems

3. Engine Thrust and Performance Parameters

3.1 Introduction

3.1.1 Takeoff Thrust

3.2 Installed Thrust--Some Bookkeeping Issues on Thrust and Drag

3.3 Engine Thrust Based on the Sum of Component Impulse

3.4 Rocket Thrust

3.5 Airbreathing Engine Performance Parameters

3.5.1 Specific Thrust

3.5.2 Specific Fuel Consumption and Specific Impulse

3.5.3 Thermal Efficiency

3.5.4 Propulsive Efficiency

3.5.5 Engine Overall Efficiency and Its Impact on Aircraft Range and Endurance

3.6 Modern Engines, Their Architecture, and Some Performance Characteristics

3.7 Summary

References

Problems

4. Gas Turbine Engine Cycle Analysis

4.1 Introduction

4.2 The Gas Generator

4.3 Aircraft Gas Turbine Engines

4.3.1 The Turbojet Engine

4.3.1.1 The Inlet

4.3.1.2 The Compressor

4.3.1.3 The Burner

4.3.1.4 The Turbine

4.3.1.5 The Nozzle

4.3.1.6 Thermal Efficiency of a Turbojet Engine

4.3.1.7 Propulsive Efficiency of a Turbojet Engine

4.3.1.8 The Overall Efficiency of a Turbojet Engine

4.3.1.9 Performance Evaluation o