Aircraft Engine Design

Εξώφυλλο
AIAA, 2002 - 692 σελίδες
3 Κριτικές
Annotation Significantly expanded and modernized, this text 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 enhanced by AEDsys software on CD-ROM that provides comprehensive computational support for every design step. 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.
 

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Περιεχόμενα

The Design Process
3
13 The Need
4
14 Our Approach
5
16 Charting the Course
6
17 Units
8
110 Looking Ahead
11
111 Example Request for Proposal
13
112 Mission Terminology
17
72 Design Tools
234
73 Engine Systems Design
238
74 Example Engine Global and Interface Quantities 741 AAF Engine Design Point Flow Properties
241
Engine Component Design Rotating Turbomachinery
253
82 Design Tools
254
Rotating Turbomachinery
299
References
323
Engine Component Design Combustion Systems
325

References
18
Constraint Analysis
19
22 Design Tools
21
23 Preliminary Estimates for Constraint Analysis
35
24 Example Constraint Analysis
39
References
54
Mission Analysis
55
32 Design Tools
57
33 Aircraft Weight and Fuel Consumption Data
70
34 Example Mission Analysis
72
References
93
Engine Selection Parametric Cycle Analysis
95
42 Design Tools
96
43 Finding Promising Solutions
117
Parametric Cycle Analysis
126
References
137
Engine Selection Performance Cycle Analysis
139
52 Design Tools
140
53 Component Behavior
163
Performance Cycle Analysis
172
References
187
Sizing the Engine Installed Performance
189
62 Design Tools
192
63 AEDsys Software Implementation of Installation Losses
206
64 Example Installed Performance and Final Engine Sizing
207
65 AAF Engine Performance
220
References
229
Engine Component Design
231
Engine Component Design Global and Interface Quantities
233
92 Design ToolsMain Burner
368
93 Design ToolsAfterburners
384
Combustion Systems
394
References
416
Engine Component Design Inlets and Exhaust Nozzles
419
103 Exhaust Nozzles
461
Inlet and Exhaust Nozzle
483
References
504
Epilogue
507
Units and Conversion Factors
509
Altitude Tables
511
Gas Turbine Engine Data
519
Engine Performance Theta Break and Throttle Ratio
523
Aircraft Engine Efficiency and Thrust Measures
537
Compressible Flow Functions for Gas with Variable Specific Heats
547
ConstantArea Mixer Analysis
551
Mixed Flow Turbofan Engine Parametric Cycle Analysis Equations
557
Mixed Flow Turbofan Engine Performance Cycle Analysis Equations
563
High Bypass Ratio Turbofan Engine Cycle Analysis
569
Turboprop Engine Cycle Analysis
589
Propeller Design Tools
609
Example Material Properties
623
Turbine Engine Life Management
635
Engine Controls
663
Global Range Airlifter GRA RFP
679
Index
681
Series Pages
689
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Δημοφιλή αποσπάσματα

Σελίδα v - Board Daniel J. Biezad Robert G. Loewy California Polytechnic State Georgia Institute of Technology University Aaron R. Byerley Michael Mohaghegh US Air Force Academy The Boeing Company Kajal K. Gupta Dora Musielak NASA Dryden Flight Research Northrop Grumman Corporation Center John K. Harvey Conrad F. Newberry Imperial College Naval Postgraduate School David K. Holger David K. Schmidt Iowa State University University of Colorado, Colorado Springs Rakesk K.
Σελίδα xv - Man's flight through life is sustained by the power of his knowledge.

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