"Aircraft Engine Design" by Jack D. Mattingly, William H. Heiser, David T. Pratt

The text presents a complete and realistic aircraft engine design experience. From the request for proposal for a new aircraft to the final engine layout, the book provides the concepts and procedures required for the entire process. It is a significantly expanded and modernized version of the best-selling first edition that emphasizes recent developments impacting engine design such as theta break/throttle ratio, life management, controls, and stealth.

The key steps of the process are detailed in 10 chapters that encompass aircraft constraint analysis, aircraft mission analysis, engine parametric (design point) analysis, engine performance (off-design) analysis, engine installation drag and sizing, and the design of inlets, fans, compressors, main combustors, turbines, afterburners, and exhaust nozzles.

Contents
Foreword
Preface
Acknowledgments
Nomenclature

Part I Engine Cycle Design
Chapter 1.The Design Process
1.1 Introduction
1.2 Designing Is Different
1.3 The Need
1.4 Our Approach
1.5 The Wheel Exists
1.6 Charting the Course
1.7 Units
1.8 The Atmosphere
1.9 Compressible Flow Relationships
1.10 Looking Ahead
1.11 Example Request for Proposal
1.12 Mission Terminology
References
Chapter 2. Constraint Analysis
2.1 Concept
2.2 Design Tools
2.3 Preliminary Estimates for Constraint Analysis
2.4 Example Constraint Analysis
References
Chapter 3. Mission Analysis
3.1 Concept
3.2 Design Tools
3.3 Aircraft Weight and Fuel Consumption Data
3.4 Example Mission Analysis
References
Chapter 4. Engine Selection: Parametric Cycle Analysis
4.1 Concept
4.2 Design Tools
4.3 Finding Promising Solutions
4.4 Example Engine Selection: Parametric Cycle Analysis
References
Chapter 5. Engine Selection: Performance Cycle Analysis
5.1 Concept
5.2 Design Tools
5.3 Component Behavior
5.4 Example Engine Selection: Performance Cycle Analysis
References
Chapter 6. Sizing the Engine: Installed Performance
6.1 Concept
6.2 Design Tools
6.3 AEDsys Software Implementation of Installation Losses
6.4 Example Installed Performance and Final Engine Sizing
6.5 AAF Engine Performance
References
Part II Engine Component Design
Chapter 7. Engine Component Design: Global and Interface
Quantities
7.1 Concept
7.2 Design Tools
7.3 Engine Systems Design
7.4 Example Engine Global and Interface Quantities
Reference
Chapter 8. Engine Component Design: Rotating
Turbomachinery
8.1 Concept
8.2 Design Tools
8.3 Example AAF Engine Component Design: Rotating
Turbomachinery
References
Chapter 9. Engine Component Design: Combustion Systems
9.1 Concept
9.2 Design Tools–Main Burner
9.3 Design Tools–Afterburners
9.4 Example Engine Component Design: Combustion Systems
References
Chapter 10Engine Component Design: Inlets and Exhaust Nozzles
10.1 Concept
10.2 Inlets
10.3 Exhaust Nozzles
10.4 Example Engine Component Design: Inlet and Exhaust Nozzle 83
References
Epilogue
Appendix A: Units and Conversion Factors
Appendix B: Altitude Tables
Appendix C: Gas lbrbine Engine Data
Appendix D: Engine Performance: Theta Break and Throttle Ratio
Appendix E: Aircraft Engine Efficiency and Thrust Measures
Appendix F: Compressible Flow Functions for Gas with Variable Specific Heats
Appendix G: Constant-Area Mixer Analysis
Appendix H: Mixed Flow Turbofan Engine Parametric Cycle Analysis Equations
Appendix I: Mixed Flow Turbofan Engine Performance Cycle Analysis Equations
Appendix J: High Bypass Ratio lbrbofan Engine Cycle Analysis
Appendix K: lbrboprop Engine Cycle Analysis
Appendix L: Propeller Design Tools
Appendix M: Example Material Properties
Appendix N: lbrbine Engine Life Management
Appendix 0: Engine Controls
Appendix P: Global Range Airlifter (GRA) RFP
Index

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