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Aircraft Design: A Systems Engineering Approach [Other digital carrier]

Series edited by (BAE Systems, UK), Series edited by (MIT), Series edited by (University of Liverpool, UK), Series edited by (Parker Aerospace Group, USA), (Daniel Webster College, USA)
  • Formaat: Other digital carrier, 808 pages, kõrgus x laius x paksus: 250x150x15 mm, kaal: 666 g
  • Sari: Aerospace Series
  • Ilmumisaeg: 19-Sep-2012
  • Kirjastus: John Wiley & Sons Inc
  • ISBN-10: 111835270X
  • ISBN-13: 9781118352700
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Aircraft Design: A Systems Engineering Approach
  • Formaat: Other digital carrier, 808 pages, kõrgus x laius x paksus: 250x150x15 mm, kaal: 666 g
  • Sari: Aerospace Series
  • Ilmumisaeg: 19-Sep-2012
  • Kirjastus: John Wiley & Sons Inc
  • ISBN-10: 111835270X
  • ISBN-13: 9781118352700
Teised raamatud teemal:
Püsilink: https://www.kriso.ee/db/9781118352700.html
Märksõnad:

A comprehensive approach to the air vehicle design process using the principles of systems engineering

Due to the high cost and the risks associated with development, complex aircraft systems have become a prime candidate for the adoption of systems engineering methodologies. This book presents the entire process of aircraft design based on a systems engineering approach from conceptual design phase, through to preliminary design phase and to detail design phase.

Presenting in one volume the methodologies behind aircraft design, this book covers the components and the issues affected by design procedures. The basic topics that are essential to the process, such as aerodynamics, flight stability and control, aero-structure, and aircraft performance are reviewed in various chapters where required.  Based on these fundamentals and design requirements, the author explains the design process in a holistic manner to emphasise the integration of the individual components into the overall design. Throughout the book the various design options are considered and weighed against each other, to give readers a practical understanding of the process overall. 

Readers with knowledge of the fundamental concepts of aerodynamics, propulsion, aero-structure, and flight dynamics will find this book ideal to progress towards the next stage in their understanding of the topic. Furthermore, the broad variety of design techniques covered ensures that readers have the freedom and flexibility to satisfy the design requirements when approaching real-world projects.

Key features:

&;         Provides full coverage of the design aspects of an air vehicle including: aeronautical concepts, design techniques and design flowcharts

&;         Features end of chapter problems to reinforce the learning process as well as fully solved design examples at component level

&;          Includes fundamental explanations for aeronautical engineering students and practicing engineers

&;          Features a solutions manual to sample questions on the book&;s companion website

Companion website -   www.wiley.com/go/sadraey

Arvustused

Summing Up: Highly recommended. All academic and technical program engineering collections. (Choice, 1 October 2013) "Readers with knowledge of the fundamental concepts of aerodynamics, propulsion, aero-structure, and flight dynamics will find this book ideal to progress towards the next stage in their understanding of the topic. Furthermore, the broad variety of design techniques covered ensures that readers have the freedom and flexibility to satisfy the design requirements when approaching real-world projects." (Expofairs.com, 25 January 2013)

Preface xv Series Preface xix Acknowledgments xxi Symbols and
Acronyms xxiii 1 Aircraft Design Fundamentals 1 1.1 Introduction to Design
1 1.2 Engineering Design 4 1.3 Design Project Planning 8 1.4 Decision
Making 10 1.5 Feasibility Analysis 12 1.6 Tort of Negligence 15 References
17 2 Systems Engineering Approach 19 2.1 Introduction 19 2.2 Fundamentals
of Systems Engineering 20 2.3 Conceptual System Design 23 2.4 Preliminary
System Design 29 2.5 Detail System Design 30 2.6 Design Requirements 33
2.7 Design Review, Evaluation, and Feedback 34 2.8 Systems Engineering
Approach in Aircraft Design 37 References 47 3 Aircraft Conceptual Design
49 3.1 Introduction 49 3.2 Primary Functions of Aircraft Components 50 3.3
Aircraft Configuration Alternatives 52 3.4 Aircraft Classification and
Design Constraints 62 3.5 Configuration Selection Process and Trade-Off
Analysis 68 3.6 Conceptual Design Optimization 74 Problems 86 References
92 4 Preliminary Design 93 4.1 Introduction 93 4.2 Maximum Take-Off Weight
Estimation 94 4.3 Wing Area and Engine Sizing 113 4.4 Design Examples 145
Problems 155 References 158 5 Wing Design 161 5.1 Introduction 161 5.2
Number of Wings 164 5.3 Wing Vertical Location 165 5.4 Airfoil Section 170
5.5 Wing Incidence 195 5.6 Aspect Ratio 198 5.7 Taper Ratio 203 5.8 The
Significance of Lift and Load Distributions 206 5.9 Sweep Angle 209 5.10
Twist Angle 223 5.11 Dihedral Angle 226 5.12 High-Lift Device 230 5.13
Aileron 241 5.14 Lifting-Line Theory 242 5.15 Accessories 246 5.16 Wing
Design Steps 249 5.17 Wing Design Example 250 Problems 259 References 264
6 Tail Design 265 6.1 Introduction 265 6.2 Aircraft Trim Requirements 268
6.4 Tail Configuration 285 6.5 Canard or Aft Tail 294 6.6 Optimum Tail Arm
298 6.7 Horizontal Tail Parameters 301 6.8 Vertical Tail Design 317 6.9
Practical Design Steps 329 6.10 Tail Design Example 331 Problems 336
References 340 7 Fuselage Design 341 7.1 Introduction 341 7.2 Functional
Analysis and Design Flowchart 341 7.3 Fuselage Configuration Design and
Internal Arrangement 345 7.4 Ergonomics 346 7.5 Cockpit Design 350 7.6
Passenger Cabin Design 360 7.7 Cargo Section Design 368 7.8 Optimum
Length-to-Diameter Ratio 372 7.9 Other Fuselage Internal Segments 380 7.10
Lofting 388 7.11 Fuselage Design Steps 394 7.12 Design Example 395
Problems 406 References 410 8 Propulsion System Design 413 8.1
Introduction 413 8.2 Functional Analysis and Design Requirements 414 8.3
Engine Type Selection 416 8.4 Number of Engines 436 8.5 Engine Location 439
8.6 Engine Installation 448 8.7 Propeller Sizing 456 8.8 Engine
Performance 461 8.9 Engine Selection 462 8.10 Propulsion System Design
Steps 464 8.11 Design Example 467 Problems 471 References 478 9 Landing
Gear Design 479 9.1 Introduction 479 9.2 Functional Analysis and Design
Requirements 481 9.3 Landing Gear Configuration 484 9.4 Fixed, Retractable,
or Separable Landing Gear 494 9.5 Landing Gear Geometry 497 9.6 Landing
Gear and Aircraft Center of Gravity 516 9.7 Landing Gear Mechanical
Subsystems/Parameters 524 9.8 Landing Gear Design Steps 528 9.9 Landing
Gear Design Example 529 Problems 539 References 544 10 Weight of
Components 547 10.1 Introduction 547 10.2 Sensitivity of Weight Calculation
549 10.3 Aircraft Major Components 553 10.4 Weight Calculation Technique
556 10.5
Chapter Examples 565 Problems 570 References 573 11 Aircraft
Weight Distribution 575 11.1 Introduction 575 11.2 Aircraft Center of
Gravity Calculation 578 11.3 Center of Gravity Range 585 11.4 Longitudinal
Center of Gravity Location 590 11.5 Technique to Determine the Aircraft
Forward and Aft Center of Gravity 598 11.6 Weight Distribution Technique 606
11.7 Aircraft Mass Moment of Inertia 615 11.8
Chapter Example 620 Problems
624 References 630 12 Design of Control Surfaces 631 12.1 Introduction 631
12.2 Configuration Selection of Control Surfaces 637 12.3 Handling
Qualities 638 12.4 Aileron Design 654 12.5 Elevator Design 670 12.6 Rudder
Design 685 12.7 Aerodynamic Balance and Mass Balance 713 12.8
Chapter
Examples 723 Problems 745 References 752 Appendices 755 Appendix A:
Standard Atmosphere, SI Units 755 Appendix B: Standard Atmosphere, British
Units 756 Index 757