did-you-know? rent-now

Amazon no longer offers textbook rentals. We do!

did-you-know? rent-now

Amazon no longer offers textbook rentals. We do!

We're the #1 textbook rental company. Let us show you why.

9781405120326

Understanding Aircraft Structures

by ;
  • ISBN13:

    9781405120326

  • ISBN10:

    1405120320

  • Edition: 4th
  • Format: Paperback
  • Copyright: 2006-02-10
  • Publisher: Wiley-Blackwell
  • Purchase Benefits
  • Free Shipping Icon Free Shipping On Orders Over $35!
    Your order must be $35 or more to qualify for free economy shipping. Bulk sales, PO's, Marketplace items, eBooks and apparel do not qualify for this offer.
  • eCampus.com Logo Get Rewarded for Ordering Your Textbooks! Enroll Now
List Price: $78.88 Save up to $0.39
  • Buy New
    $78.49
    Add to Cart Free Shipping Icon Free Shipping

    PRINT ON DEMAND: 2-4 WEEKS. THIS ITEM CANNOT BE CANCELLED OR RETURNED.

Supplemental Materials

What is included with this book?

Summary

This book explains aircraft structures so as to provide a basic understanding of the subject and the terminology used, as well as illustrating some of the problems. It provides a brief historical background, and covers parts of the aeroplane, loads, structural form, materials, processes, detail design, quality control, stressing, and the documentation associated with modification and repairs. The Fourth Edition takes account of new materials and the new European regulatory system.

Author Biography

John Cutler is a consulting engineer, a Fellow of the Royal Aeronautical Society and a Chartered Engineer.


Jeremy Liber, who has been responsible for revising the Fourth Edition, has worked in the fixed and rotary wing aircraft industry for a number of years as a stressman, structural test engineer and design engineer. He has degrees in both engineering and business plus a pilot’s licence. He is a Member of the Royal Aeronautical Society and is currently Technical Director at Britten-Norman Aircraft Ltd.

Table of Contents

Preface ix
Chapter 1 Introduction 1(2)
Chapter 2 History 3(26)
2.1 Outline
3(1)
2.2 Wire-braced structures
4(5)
2.3 Semi-monocoque structures
9(5)
2.4 Sandwich structures
14(1)
2.5 Review of the key points
15(14)
Chapter 3 Parts of the Aircraft 29(9)
3.1 Terms connected with flight
29(2)
3.2 Terms connected with control
31(1)
3.3 Terms connected with high-lift devices
32(1)
3.4 Terms associated with the shape and dimensions of the aircraft
32(5)
3.5 Review of the key points
37(1)
Chapter 4 Loads on the Aircraft 38(19)
4.1 General flight forces
38(6)
4.2 Acceleration loads
44(4)
4.3 Further aerodynamic loads
48(2)
4.4 Other loads
50(1)
4.5 Further load factors
51(2)
4.6 Loads acting on the whole aircraft
53(2)
4.7 Review of the key points
55(1)
4.8 References
56(1)
Chapter 5 The Form of Structures 57(32)
5.1 Structure relative to aircraft design
57(1)
5.2 Historic form of structure
57(2)
5.3 General form of structure
59(1)
5.4 The basic load systems in structures
59(4)
5.5 The forms of stress in materials
63(9)
5.6 Bending and torsion
72(13)
5.7 Compression
85(2)
5.8 The whole structure
87(1)
5.9 Review of the key points
87(1)
5.10 References
88(1)
Chapter 6 Materials 89(23)
6.1 Choice of materials
89(3)
6.2 Material properties
92(9)
6.3 Smart structures (and materials)
101(2)
6.4 Cost as a property of a material
103(2)
6.5 Heat treatment
105(1)
6.6 Reference number for materials
106(3)
6.7 Review of the key points
109(1)
6.8 References
110(2)
Chapter 7 Processes 112(12)
7.1 Introduction
112(1)
7.2 Manufacturing
112(7)
7.3 Jointing
119(4)
7.4 Review of the key points
123(1)
7.5 References
123(1)
Chapter 8 Corrosion and Protective Treatments 124(9)
8.1 Nature of corrosion
124(2)
8.2 Causes of corrosion
126(2)
8.3 Protection against corrosion
128(4)
8.4 Review of the key points
132(1)
8.5 Reference
132(1)
Chapter 9 Detail Design 133(26)
9.1 Sheet-metal components
133(3)
9.2 Machined components and large forgings
136(3)
9.3 Notching and stress raisers
139(5)
9.4 Rivets and bolts
144(8)
9.5 Joggling
152(2)
9.6 Clips or cleats
154(1)
9.7 Stringer/frame intersections
155(1)
9.8 Lugs
156(1)
9.9 The 'stiff path'
157(1)
9.10 Review of the key points
157(2)
Chapter 10 Composite Materials in Aircraft Structures 159(14)
10.1 What are composites?
159(2)
10.2 The strength of composite materials
161(1)
10.3 Types of structures
162(2)
10.4 Joining composites
164(3)
10.5 Fibres
167(2)
10.6 Resins
169(2)
10.7 Working safely with composites
171(1)
10.8 Review of the key points
172(1)
Chapter 11 Quality and Airworthiness 173(9)
11.1 Quality assurance and quality control
173(1)
11.2 Control
174(1)
11.3 Procedures and systems
175(2)
11.4 Further notes on quality control functions
177(2)
11.5 Airworthiness engineering
179(1)
11.6 Continued airworthiness
180(1)
11.7 Review of the key points
181(1)
11.8 References
181(1)
Chapter 12 Stressing 182(13)
12.1 Introduction
182(1)
12.2 The stressman's work
183(4)
12.3 Stressing methods
187(3)
12.4 Stress reports
190(3)
12.5 Review of the key points
193(1)
12.6 References
194(1)
Chapter 13 Presentation of Modifications and Repairs 195(8)
13.1 Definitions
195(2)
13.2 The essential paperwork associated with modifications
197(4)
13.3 Review of the key points
201(1)
13.4 Conclusion
201(1)
13.5 References
202(1)
Appendices 203(6)
Index 209

Supplemental Materials

What is included with this book?

The New copy of this book will include any supplemental materials advertised. Please check the title of the book to determine if it should include any access cards, study guides, lab manuals, CDs, etc.

The Used, Rental and eBook copies of this book are not guaranteed to include any supplemental materials. Typically, only the book itself is included. This is true even if the title states it includes any access cards, study guides, lab manuals, CDs, etc.

Rewards Program