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Sun, C. T.
Mechanics of Aircraft Structures

2. Edition - June 2006
129.- Euro
2006. 320 Pages, Hardcover
ISBN-10: 0-471-69966-7
ISBN-13: 978-0-471-69966-8 - John Wiley & Sons


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Sample Chapter

Short description
Mechanics of Aircraft Structures, Second Edition is the revised update of the original bestselling textbook about aerospace engineering. This book covers the materials and analysis tools used for aircraft structural design and mechanics in the same easy to understand manner. The new edition focuses on three levels of coverage driven by recent advances in industry: the increase in the use of commercial finite element codes require an improved capability in students to formulate the problem and develop a judgement of the accuracy of the numerical results; the focus on fracture mechanics as a tool in studying damage tolerance and durability has made it necessary to introduce students at the undergraduate level to this subject; a new class of materials including advanced composites, are very different from the traditional metallic materials, requiring students and practitioners to understand the advantages the new materials make possible. This new edition will provide more homework problems for each chapter, more examples, and more details in some of the derivations.

From the contents
Preface.

Preface to the First Edition.

1 Characteristics of Aircraft Structures and Materials.

1.1 Introduction.

1.2 Basic Structural Elements in Aircraft Structure.

1.3 Wing and Fuselage.

1.4 Aircraft Materials.

Problems.

2 Introduction to Elasticity.

2.1 Concept of Displacement.

2.2 Strain.

2.3 Stress.

2.4 Equations of Equilibrium in a Nonuniform Stress Field.

2.5 Principal Stress.

2.6 Shear Stress.

2.7 Revisit of Transformation of Stress.

2.8 Linear Stress-Strain Relations.

2.9 Elastic Strain Energy.

2.10 Plane Elasticity.

Problems.

3 Torsion.

3.1 Saint-Venant's Principle.

3.2 Torsion of Uniform Bars.

3.3 Bars with Circular Cross-Sections.

3.4 Bars with Narrow Rectangular Cross-Sections.

3.5 Closed Single-Cell Thin-Walled Sections.

3.6 Multicell Thin-Walled Sections.

3.7 Warping in Open Thin-Walled Sections.

3.8 Warping in Closed Thin-Walled Sections.

3.9 Effect of End Constraints.

Problems.

4 Bending and Flexural Shear.

4.1 Derivation of the Simple (Bernoulli-Euler) Beam Equation.

4.2 Bidirectional Bending.

4.3 Transverse Shear Stress due to Transverse Force in Symmetric Sections.

4.4 Timoshenko Beam Theory.

4.5 Shear Lag.

Problems.

5 Flexural Shear Flow in Thin-Walled Sections.

5.1 Flexural Shear Flow in Open Thin-Walled Sections.

5.2 Shear Center in Open Sections.

5.3 Closed Thin-Walled Sections and Combined Flexural and Torsional Shear Flow.

5.4 Closed Multicell Sections.

Problems.

6 Failure Criteria for Isotropic Materials.

6.1 Strength Criteria for Brittle Materials.

6.2 Yield Criteria for Ductile Materials.

6.3 Fracture Mechanics.

6.4 Stress Intensity Factor.

6.5 Effect of Crack Tip Plasticity.

6.6 Fatigue Failure.

6.7 Fatigue Crack Growth.

Problems.

7 Elastic Buckling.

7.1 Eccentrically Loaded Beam-Column.

7.2 Elastic Buckling of Straight Bars.

7.3 Initial Imperfection.

7.4 Postbuckling Behavior.

7.5 Bar of Unsymmetric Section.

7.6 Torsional-Flexural Buckling of Thin-Walled Bars.

7.7 Elastic Buckling of Flat Plates.

7.8 Local Buckling of Open Sections.

Problems.

8 Analysis of Composite Laminates.

8.1 Plane Stress Equations for Composite Lamina.

8.2 Off-Axis Loading.

8.3 Notation for Stacking Sequence in Laminates.

8.4 Symmetric Laminate under In-Plane Loading.

8.5 Effective Moduli for Symmetric Laminates.

8.6 Laminar Stresses.

8.7 [±45°] Laminate.

Problems.

Index.


 
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