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Aircraft Engine Design 2nd Revised edition [Multiple-component retail product]

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  • Formāts: Multiple-component retail product, 600 pages, height: 230 mm
  • Izdošanas datums: 15-Aug-2003
  • Izdevniecība: American Institute of Aeronautics & Astronautics
  • ISBN-10: 1563475383
  • ISBN-13: 9781563475382
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  • Multiple-component retail product
  • Cena: 108,03 €
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Aircraft Engine Design 2nd Revised editionPalielināt
  • Formāts: Multiple-component retail product, 600 pages, height: 230 mm
  • Izdošanas datums: 15-Aug-2003
  • Izdevniecība: American Institute of Aeronautics & Astronautics
  • ISBN-10: 1563475383
  • ISBN-13: 9781563475382
Citas grāmatas par šo tēmu:
Permanent link: https://www.kriso.lv/db/9781563475382.html
Keywords:
This 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 an expanded and updated version of the first edition that emphasizes contemporary developments impacting engine design such as theta break/throttle ratio, life management, controls, and stealth. The key steps of the process are detailed in ten 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. The AEDsys software that accompanies the text provides comprehensive computational support for every design step. The software has been carefully integrated with the text to enhance both the learning process and productivity, and allows effortless transfer between British Engineering and SI units. The AEDsys software is furnished on CD and runs in the Windows operating system on PC-compatible systems.A user's manual is provided with the software, along with the complete data files used for the Air-to-Air Fighter and Global Range Airlifter design examples of the book.
Foreword vii
Preface xiii
Acknowledgments xvii
Nomenclature xix
Part I Engine Cycle Design
The Design Process
3(16)
Introduction
3(1)
Designing Is Different
3(1)
The Need
4(1)
Our Approach
5(1)
The Wheel Exists
5(1)
Charting the Course
6(2)
Units
8(1)
The Atmosphere
8(1)
Compressible Flow Relationships
8(3)
Looking Ahead
11(2)
Example Request for Proposal
13(4)
Mission Terminology
17(2)
References
18(1)
Constraint Analysis
19(36)
Concept
19(2)
Design Tools
21(14)
Preliminary Estimates for Constraint Analysis
35(4)
Example Constraint Analysis
39(16)
References
54(1)
Mission Analysis
55(40)
Concept
55(2)
Design Tools
57(13)
Aircraft Weight and Fuel Consumption Data
70(2)
Example Mission Analysis
72(23)
References
93(2)
Engine Selection: Parametric Cycle Analysis
95(44)
Concept
95(1)
Design Tools
96(21)
Finding Promising Solutions
117(9)
Example Engine Selection: Parametric Cycle Analysis
126(13)
References
137(2)
Engine Selection: Performance Cycle Analysis
139(50)
Concept
139(1)
Design Tools
140(23)
Component Behavior
163(9)
Example Engine Selection: Performance Cycle Analysis
172(17)
References
187(2)
Sizing the Engine: Installed Performance
189(44)
Concept
189(3)
Design Tools
192(14)
AEDsys Software Implementation of Installation Losses
206(1)
Example Installed Performance and Final Engine Sizing
207(13)
AAF Engine Performance
220(13)
References
229(4)
Part II Engine Component Design
Engine Component Design: Global and Interface Quantities
233(20)
Concept
233(1)
Design Tools
234(4)
Engine Systems Design
238(3)
Example Engine Global and Interface Quantities
241(12)
Reference
251(2)
Engine Component Design: Rotating Turbomachinery
253(72)
Concept
253(1)
Design Tools
254(45)
Example AAF Engine Component Design: Rotating Turbomachinery
299(26)
References
323(2)
Engine Component Design: Combustion Systems
325(94)
Concept
325(43)
Design Tools---Main Burner
368(16)
Design Tools---Afterburners
384(10)
Example Engine Component Design: Combustion Systems
394(25)
References
416(3)
Engine Component Design: Inlets and Exhaust Nozzles
419(88)
Concept
419(1)
Inlets
419(42)
Exhaust Nozzles
461(22)
Example Engine Component Design: Inlet and Exhaust Nozzle
483(24)
References
504(3)
Epilogue 507(2)
Appendix A: Units and Conversion Factors 509(2)
Appendix B: Altitude Tables 511(8)
Appendix C: Gas Turbine Engine Data 519(4)
Appendix D: Engine Performance: Theta Break and Throttle Ratio 523(14)
Appendix E: Aircraft Engine Efficiency and Thrust Measures 537(10)
Appendix F: Compressible Flow Functions for Gas with Variable Specific Heats 547(4)
Appendix G: Constant-Area Mixer Analysis 551(6)
Appendix H: Mixed Flow Turbofan Engine Parametric Cycle Analysis Equations 557(6)
Appendix I: Mixed Flow Turbofan Engine Performance Cycle Analysis Equations 563(6)
Appendix J: High Bypass Ratio Turbofan Engine Cycle Analysis 569(20)
Appendix K: Turboprop Engine Cycle Analysis 589(20)
Appendix L: Propeller Design Tools 609(14)
Appendix M: Example Material Properties 623(12)
Appendix N: Turbine Engine Life Management 635(28)
Appendix O: Engine Controls 663(16)
Appendix P: Global Range Airlifter (GRA) RFP 679(2)
Index 681(8)
Series Pages 689