Atjaunināt sīkdatņu piekrišanu

Aircraft Engine Design 3rd edition [Hardback]

4.19/5 (16 ratings by Goodreads)
, , , ,
  • Formāts: Hardback, 834 pages
  • Sērija : AIAA Education Series
  • Izdošanas datums: 06-Jun-2019
  • Izdevniecība: American Institute of Aeronautics & Astronautics
  • ISBN-10: 1624105173
  • ISBN-13: 9781624105173
Citas grāmatas par šo tēmu:
  • Hardback
  • Cena: 91,26 €*
  • * ši ir gala cena, t.i., netiek piemērotas nekādas papildus atlaides
  • atlaide spēkā tikai noliktavā esošajiem eksemplāriem (cena pasūtot jaunu: 124,94 €)
  • Standarta cena: 124,94 €
  • Ietaupiet 27%
  • Noliktavā 1 eksempl.
  • Daudzums:
  • Ielikt grozā
  • Pievienot vēlmju sarakstam
Aircraft Engine Design 3rd editionPalielināt
  • Formāts: Hardback, 834 pages
  • Sērija : AIAA Education Series
  • Izdošanas datums: 06-Jun-2019
  • Izdevniecība: American Institute of Aeronautics & Astronautics
  • ISBN-10: 1624105173
  • ISBN-13: 9781624105173
Citas grāmatas par šo tēmu:
Permanent link: https://www.kriso.lv/db/9781624105173.html
Keywords:
Aircraft Engine Design, Third Edition presents a complete and realistic aircraft engine design experience. From the request for proposal for a new aircraft to the final engine layout, it outlines the concepts and procedures required for the entire process. The writing of the third edition of Aircraft Engine Design began as soon as the second edition was published in 2003. The ensuing 15 years of evolutionary changes have created an improved, new work. The special contributions of uniquely qualied experts continue to provide valuable material to this new edition. These include Appendix L on Turbine Engine Life Management by Dr. William D. Cowie and Appendix M on Engine Controls by Charles A. Skira (with Timothy J. Lewis and Zane D. Gastineau) with update by Dr. Link Jaw.
Preface to the Third Edition xi
Preface to the Second Edition xiii
Acknowledgments xvii
Nomenclature xix
PART I Engine Cycle Design
Chapter 1 The Design Process
1(22)
1.1 IntroductiorK
1(1)
1.2 Designing is Different
2(1)
1.3 The Requirements
2(2)
1.4 Our Approach
4(1)
1.5 The Engine Design Process Exists
5(1)
1.6 Charting the Course
5(2)
1.7 Units
7(1)
1.8 The Atmosphere
8(1)
1.9 Compressible Flow Relationships
8(6)
1.10 Looking Ahead
14(3)
1.11 Example Request for Proposal
17(4)
1.12 Mission Terminology
21(2)
References
22(1)
Chapter 2 Aircraft/Engine System Constraint Analysis
23(44)
2.1 Concept
23(2)
2.2 Design Tools
25(17)
2.3 Preliminary Estimates for Constraint Analysis
42(7)
2.4 Example Constraint Analysis
49(18)
References
65(2)
Chapter 3 Aircraft/Engine System Mission Analysis
67(50)
3.1 Concept
67(2)
3.2 Design Tools
69(18)
3.3 Aircraft Weight and Fuel Consumption Estimation
87(4)
3.4 Example Mission Analysis
91(26)
References
116(1)
Chapter 4 Engine Selection: Parametric Cycle Analysis
117(46)
4.1 Concept
117(2)
4.2 Design Tools
119(23)
4.3 Finding Promising Solutions
142(8)
4.4 Example Parametric Cycle Analysis
150(13)
References
162(1)
Chapter 5 Engine Selection: Engine Performance Analysis
163(58)
5.1 Concept
163(1)
5.2 Design Tools: Modified Specific Heat (MSH) Gas Model
164(22)
5.3 Component Behavior
186(11)
5.4 Design Steps Using AEDsys Programs
197(4)
5.5 Example Engine Selection: AAF Performance Cycle Analysis
201(20)
References
218(3)
Chapter 6 Sizing the Engine: Installed Performance
221(52)
6.1 Concept
221(3)
6.2 Design Tools
224(18)
6.3 AEDsys Software Implementation of Installation Losses
242(2)
6.4 Example Installed Performance and Final Engine Sizing
244(15)
6.5 AAF Engine Performance
259(14)
References
271(2)
PART II Engine Component Design
Chapter 7 Engine Component Design: Global and Interface Quantities
273(24)
7.1 Concept
273(1)
7.2 Design Tools
274(6)
7.3 Engine Systems Design
280(4)
7.4 Example Engine Global and Interface Quantities
284(13)
References
296(1)
Chapter 8 Engine Component Design: Turbomachinery
297(90)
8.1 Concept
297(1)
8.2 Design Tools
298(59)
8.3 Example AAF Engine Component Design: Turbomachinery
357(30)
References
384(3)
Chapter 9 Engine Component Design: Combustion Systems
387(114)
9.1 Concept
387(7)
9.2 Design Tools
394(78)
9.3 Example AAF Engine Component Design: Combustion Systems
472(29)
References
499(2)
Chapter 10 Engine Component Design: Inlets and Exhaust Nozzles
501(112)
10.1 Concept
501(1)
10.2 Inlets
501(57)
10.3 Exhaust Nozzles
558(28)
10.4 Example Engine Component Design: Inlet and Exhaust Nozzle
586(27)
References
611(2)
Appendix A Units and Conversion Factors 613(2)
Appendix B Altitude Tables 615(8)
Appendix C Gas Turbine Engine Data: Uninstalled Performance 623(10)
Appendix D Engine Performance: Theta Break and Throttle Ratio 633(20)
Appendix E Aircraft Engine Efficiency and Thrust Measures 653(12)
Appendix F Mixed Flow Turbofan Engine Parametric Cycle Analysis Equations 665(6)
Appendix G Mixed Flow Turbofan Engine Performance Cycle Analysis Equations 671(8)
Appendix H High Bypass Ratio Turbofan Engine Cycle Analysis 679(26)
Appendix I Turboprop Turboshaft Engine 705(28)
Appendix J Propeller Design Tools 733(16)
Appendix K Example Material Properties 749(14)
Appendix L Turbine Engine Life Management 763(32)
Appendix M Engine Controls 795(18)
Appendix N Global Range Airlifter (GRA) RFP 813(2)
Index 815(18)
About the Authors 833(2)
Supporting Materials 835