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9781563472817

Aircraft Design : A Conceptual Approach

by
  • ISBN13:

    9781563472817

  • ISBN10:

    1563472813

  • Edition: 3rd
  • Format: Hardcover
  • Copyright: 1999-08-01
  • Publisher: Amer Inst of Aeronautics &
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List Price: $105.95

Summary

This highly regarded textbook presents the entire process of aircraft conceptual design--from requirements definition to initial sizing, configuration layout, analysis, sizing, and trade studies--in the same manner seen in industry aircraft design groups. The book has more than 900 pages of design methods, illustrations, tips, explanations, and equations, and has extensive appendices with key data essential to design. With the third edition, Raymer has updated his book to reflect the latest advances in technologies such as hypersonics, stealth, and STOVL, and the newest design methods including concurrent engineering, cost as an independent variable, and the impact of the factory of the future. Expanded are treatments of such key areas as jet engine installation, CFD, trim analysis, CAD/CAM, propeller thrust analysis, weights estimation, cost analysis, and multivariable optimization. A step-by-step description of how a typical design is developed (with illustrations) is included, and also describes the technical concepts behind some unusual design approaches su

Table of Contents

Author's Note xvii
Design---A Separate Discipline
What Is Design?
1(1)
Introduction to the Book
1(2)
Overview of the Design Process
Introduction
3(1)
Phases of Aircraft Design
3(5)
Aircraft Conceptual Design Process
8(4)
Integrated Product Development and Aircraft Design
12(3)
Sizing from a Conceptual sketch
Introduction
15(1)
Takeoff-Weight Buildup
15(1)
Empty-Weight Estimation
16(1)
Fuel-Fraction Estimation
17(10)
Takeoff-Weight Calculation
27(2)
Design Example: Asw Aircraft
29(10)
Airfoil and Geometry Selection
Introduction
39(1)
Airfoil Selection
39(15)
Wing Geometry
54(20)
Biplane Wings
74(2)
Tail Geometry and Arrangement
76(11)
Thrust-to-Weight Ratio and Wing Loading
Introduction
87(1)
Thrust-to-Weight Ratio
88(6)
Wing Loading
94(17)
Selection of Thrust-to-Weight and Wing Loading
111(2)
Initial Sizing
Introduction
113(1)
Rubber-Engine Sizing
114(7)
Fixed-Engine Sizing
121(1)
Geometry Sizing
122(4)
Control-Surface Sizing
126(5)
Configuration Layout and Loft
Introduction
131(1)
End Products of Configuration Layout
131(5)
Conic Lofting
136(6)
Conic Fuselage Development
142(7)
Flat-Wrap Fuselage Lofting
149(2)
Circle-to-Square Adapter
151(2)
Fuselage Loft Verification
153(2)
Wing/Tail Layout and Loft
155(11)
Wetted Area Determination
166(2)
Volume Determination
168(1)
Use of CAD in Conceptual Design
169(6)
Special Considerations in Configuration Layout
Introduction
175(1)
Aerodynamic Considerations
175(8)
Structural Considerations
183(8)
Radar Detectability
191(10)
Infrared Detectability
201(1)
Visual Detectability
201(1)
Aural Signature
202(1)
Vulnerability Considerations
203(2)
Crashworthiness Considerations
205(1)
Producibility Considerations
206(5)
Maintainability Considerations
211(4)
Crew Station, Passengers, and Payload
Introduction
215(1)
Crew Station
215(4)
Passenger compartment
219(1)
Cargo Provisions
220(2)
Weapons Carriage
222(4)
Gun Installation
226(3)
Propulsion and Fuel System Integration
Introduction
229(1)
Propulsion Selection
229(3)
Jet-Engine Integration
232(28)
Propeller-Engine Integration
260(7)
Fuel System
267(4)
Landing Gear and Subsystems
Introduction
271(1)
Landing Gear Arrangements
271(5)
Tire Sizing
276(7)
Shock Absorbers
283(7)
Castoring-Wheel Geometry
290(1)
Gear-Retraction Geometry
291(3)
Seaplanes
294(2)
Subsystems
296(11)
INTERMISSION: STEP-BY-STEP DEVELOPMENT OF A NEW DESIGN 307(472)
Aerodynamics
Introduction
315(1)
Aerodynamic Forces
315(5)
Aerodynamic Coefficients
320(2)
Lift
322(18)
Parasite (Zero-Lift) Drag
340(19)
Drag Due to Lift (Induced Drag)
359(9)
Aerodynamic Codes and Computational Fluid Dynamics (CFD)
368(11)
Propulsion
Introduction
379(2)
Jet-Engine Thrust Considerations
381(3)
Turbojet Installed Thrust
384(1)
Thrust-Drag Bookkeeping
384(1)
Installed-Thrust Methodology
385(8)
Piston-Engine Performance
393(7)
Turboprop Performance
400(3)
Structures and Loads
Introduction
403(1)
Loads Categories
404(2)
Air Loads
406(11)
Inertial Loads
417(1)
Powerplant Loads
418(1)
Landing-Gear Loads
418(1)
Structures Fundamentals
419(6)
Material Selection
425(3)
Material Properties
428(13)
Structural-Analysis Fundamentals
441(20)
Finite-Element Structural Analysis
461(6)
Weights
Introduction
467(3)
Approximate Group Weights Method
470(1)
Statistical Group Weights Method
470(9)
Additional Considerations in Weights Estimation
479(2)
Stability, Control, and Handling Qualities
Introduction
481(2)
Coordinate Systems and Definitions
483(1)
Longitudinal Static Stability and Control
484(21)
Lateral-Directional Static Stability and Control
505(9)
Stick-Free Stability
514(1)
Effects of Flexibility
514(2)
Dynamic Stability
516(4)
Quasi-Steady State
520(2)
Inertia Coupling
522(1)
Handling Qualities
523(8)
Performance and Flight Mechanics
Introduction and Equations of Motion
531(1)
Steady Level Flight
532(9)
Steady Climbing and Descending Flight
541(4)
Level Turning Flight
545(3)
Gliding Flight
548(4)
Energy-Maneuverability Methods
552(9)
Operating Envelope
561(2)
Takeoff Analysis
563(4)
Landing Analysis
567(2)
Other Fighter Performance Measures of Merit
569(10)
Cost Analysis
Introduction
579(1)
Elements of Life-Cycle Cost
580(3)
Cost-Estimating Methods
583(1)
RDT&E and Production Costs
584(5)
Operations and Maintenance Costs
589(4)
Cost Measures of Merit (Military)
593(1)
Aircraft and Airline Economics
593(4)
Sizing and Trade Studies
Introduction
597(1)
Detailed Sizing Methods
597(1)
Improved Conceptual Sizing Methods
598(5)
Sizing Matrix and Carpet Plots
603(7)
Trade Studies
610(7)
Design of Unique Aircraft Concepts
Introduction
617(1)
Jet VTOL
617(22)
Prop VTOL and Helicopter
639(18)
Hypersonic Vehicles
657(4)
Flying Wing, Tailless, Lifting Fuselage, and Blended Wing-Body
661(3)
Delta and Double-Delta Wing
664(3)
Forward-Swept Wing
667(2)
Canard-Pusher
669(1)
Multi-Fuselage
670(2)
Asymmetrical
672(4)
Joined Wing
676(1)
Wing-in-Ground Effect
677(2)
Unmanned/Uninhabited
679(2)
Conceptual Design Examples
Introduction
681(1)
Single-Seat Aerobatic
682(44)
Lightweight Supercruise Fighter
726(53)
Appendix A. Unit Conversion 779(40)
Appendix B. Standard Atmosphere, Compressible Flow, and Shocks
B.1 Standard Atmosphere
784(4)
B.2 Compressible Flow Tables
788(12)
B.3 Shock Charts
800(15)
Appendix C. Airspeed
C.1 Airspeed Relationships
815(1)
C.2 Airspeed Conversion Charts
816(3)
Appendix D. Airfoil Data 819(48)
Appendix E. Typical Engine Performance Curves
E.1 Afterburning Turbofan
853(6)
E.2 High-Bypass Turbofan
859(4)
E.3 Turboprop
863(4)
Appendix F. Design Requirements and Specifications 867(6)
References 873(6)
Questions 879(10)
Index 889

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