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Introduction to Aircraft Structural Analysis - 2nd Edition - ISBN: 9780080982014, 9780080982038

Introduction to Aircraft Structural Analysis

2nd Edition

Author: T.H.G. Megson
eBook ISBN: 9780080982038
Imprint: Butterworth-Heinemann
Published Date: 22nd October 2013
Page Count: 728
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Introduction to Aircraft Structural Analysis, Second Edition, is an essential resource for learning aircraft structural analysis. Based on the author's best-selling text Aircraft Structures for Engineering Students, this brief book covers the basics of structural analysis as applied to aircraft structures.

Coverage of elasticity, energy methods, and virtual work sets the stage for discussions of airworthiness/airframe loads and stress analysis of aircraft components. Numerous worked examples, illustrations, and sample problems show how to apply the concepts to realistic situations.

This text is designed for undergraduate and postgraduate students of aerospace and aeronautical engineering as well as for professional development and training courses.

Key Features

  • Based on the author's best-selling text Aircraft Structures for Engineering Students, this introduction covers core concepts in about 200 fewer pages than the original by removing some optional topics like structural vibrations and aeroelasticity
  • Systematic step-by-step procedures in the worked examples
  • Self-contained, with complete derivations for key equations


Undergraduate and postgraduate students of aerospace and aeronautical engineering. Also suitable for professional development and training courses

Table of Contents


Part A: Fundamentals of structural analysis

Section A1. Elasticity

Chapter 1. Basic elasticity

1.1 Stress

1.2 Notation for forces and stresses

1.3 Equations of equilibrium

1.4 Plane stress

1.5 Boundary conditions

1.6 Determination of stresses on inclined planes

1.7 Principal stresses

1.8 Mohr’s circle of stress

1.9 Strain

1.10 Compatibility equations

1.11 Plane strain

1.12 Determination of strains on inclined planes

1.13 Principal strains

1.14 Mohr’s circle of strain

1.15 Stress–strain relationships

1.16 Experimental measurement of surface strains


Additional Reading


Chapter 2. Two-dimensional problems in elasticity

2.1 Two-dimensional problems

2.2 Stress functions

2.3 Inverse and semi-inverse methods

2.4 St. Venant’s principle

2.5 Displacements

2.6 Bending of an end-loaded cantilever



Chapter 3. Torsion of solid sections

3.1 Prandtl stress function solution

3.2 St. Venant warping function solution

3.3 The membrane analogy

3.4 Torsion of a narrow rectangular strip



Section A2. Virtual work, energy, and matrix methods

Chapter 4. Virtual work and energy methods

4.1 Work

4.2 Principle of virtual work

4.3 Applications of the principle of virtual work



Chapter 5. Energy methods

5.1 Strain energy and complementary energy

5.2 Principle of the stationary value of the total complementary energy

5.3 Application to deflection problems

5.4 Application to the solution of statically indeterminate systems

5.5 Unit load method

5.6 Flexibility method

5.7 Total potential energy

5.8 Principle of the stationary value of the total potential energy

5.9 Principle of superposition

5.10 Reciprocal theorem

5.11 Temperature effects


Further reading


Chapter 6. Matrix methods

6.1 Notation

6.2 Stiffness matrix for an elastic spring

6.3 Stiffness matrix for two elastic springs in line

6.4 Matrix analysis of pin-jointed frameworks

6.5 Application to statically indeterminate frameworks

6.6 Matrix analysis of space frames

6.7 Stiffness matrix for a uniform beam

6.8 Finite element method for continuum structures


Further reading


Section A3. Thin plate theory

Chapter 7. Bending of thin plates

7.1 Pure bending of thin plates

7.2 Plates subjected to bending and twisting

7.3 Plates subjected to a distributed transverse load

7.4 Combined bending and in-plane loading of a thin rectangular plate

7.5 Bending of thin plates having a small initial curvature

7.6 Energy method for the bending of thin plates

Further reading


Section A4. Structural instability

Chapter 8. Columns

8.1 Euler buckling of columns

8.2 Inelastic buckling

8.3 Effect of initial imperfections

8.4 Stability of beams under transverse and axial loads

8.5 Energy method for the calculation of buckling loads in columns

8.6 Flexural–torsional buckling of thin-walled columns



Chapter 9. Thin plates

9.1 Buckling of thin plates

9.2 Inelastic buckling of plates

9.3 Experimental determination of the critical load for a flat plate

9.4 Local instability

9.5 Instability of stiffened panels

9.6 Failure stress in plates and stiffened panels

9.7 Tension field beams



Part B: Analysis of aircraft structures

Section B1. Principles of stressed skin construction

Chapter 10. Materials

10.1 Aluminum alloys

10.2 Steel

10.3 Titanium

10.4 Plastics

10.5 Glass

10.6 Composite materials

10.7 Properties of materials


Chapter 11. Structural components of aircraft

11.1 Loads on structural components

11.2 Function of structural components

11.3 Fabrication of structural components

11.4 Connections



Section B2. Airworthiness and airframe loads

Chapter 12. Airworthiness

12.1 Factors of safety-flight envelope

12.2 Load factor determination



Chapter 13. Airframe loads

13.1 Aircraft inertia loads

13.2 Symmetric maneuver loads

13.3 Normal accelerations associated with various types of maneuver

13.4 Gust loads



Chapter 14. Fatigue

14.1 Safe life and fail-safe structures

14.2 Designing against fatigue

14.3 Fatigue strength of components

14.4 Prediction of aircraft fatigue life

14.5 Crack propagation


Further reading


Section B3. Bending, shear and torsion of thin-walled beams

Chapter 15. Bending of open and closed, thin-walled beams

15.1 Symmetrical bending

15.2 Unsymmetrical bending

15.3 Deflections due to bending

15.4 Calculation of section properties

15.5 Applicability of bending theory

15.6 Temperature effects



Chapter 16. Shear of beams

16.1 General stress, strain, and displacement relationships for open and single-cell closed section thin-walled beams

16.2 Shear of open section beams

16.3 Shear of closed section beams



Chapter 17. Torsion of beams

17.1 Torsion of closed section beams

17.2 Torsion of open section beams


Chapter 18. Combined open and closed section beams

18.1 Bending

18.2 Shear

18.3 Torsion


Chapter 19. Structural idealization

19.1 Principle

19.2 Idealization of a panel

19.3 Effect of idealization on the analysis of open and closed section beams

19.4 Deflection of open and closed section beams


Section B4. Stress analysis of aircraft components

Chapter 20. Wing spars and box beams

20.1 Tapered wing spar

20.2 Open and closed section beams

20.3 Beams having variable stringer areas


Chapter 21. Fuselages

21.1 Bending

21.2 Shear

21.3 Torsion

21.4 Cut-outs in fuselages


Chapter 22. Wings

22.1 Three-boom shell

22.2 Bending

22.3 Torsion

22.4 Shear

22.5 Shear center

22.6 Tapered wings

22.7 Deflections

22.8 Cut-outs in wings


Chapter 23. Fuselage frames and wing ribs

23.1 Principles of stiffener/web construction

23.2 Fuselage frames

23.3 Wing ribs


Chapter 24. Laminated composite structures

24.1 Elastic constants of a simple lamina

24.2 Stress–strain relationships for an orthotropic ply (macro approach)

24.3 Thin-walled composite beams





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© Butterworth-Heinemann 2013
22nd October 2013
eBook ISBN:

About the Author

T.H.G. Megson

T.H.G. Megson is a professor emeritus with the Department of Civil Engineering at Leeds University (UK). For Elsevier he has written the market leading Butterworth Heinemann textbooks Aircraft Structures for Engineering Students and Introduction to Aircraft Structural Analysis (a briefer derivative of the aircraft structures book), as well as the text/ref hybrid Structural and Stress Analysis.

Affiliations and Expertise

Department of Civil Engineering, Leeds University, UK

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