Mechanics of Aircraft Structures

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9780471699668: Mechanics of Aircraft Structures
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Designed to help students get a solid background in structural mechanics and extensively updated to help professionals get up to speed on recent advances This Second Edition of the bestselling textbook Mechanics of Aircraft Structures combines fundamentals, an overview of new materials, and rigorous analysis tools into an excellent one-semester introductory course in structural mechanics and aerospace engineering. It's also extremely useful to practicing aerospace or mechanical engineers who want to keep abreast of new materials and recent advances. Updated and expanded, this hands-on reference covers: Introduction to elasticity of anisotropic solids, including mechanics of composite materials and laminated structures Stress analysis of thin-walled structures with end constraints Elastic buckling of beam-column, plates, and thin-walled bars Fracture mechanics as a tool in studying damage tolerance and durability Designed and structured to provide a solid foundation in structural mechanics, Mechanics of Aircraft Structures, Second Edition includes more examples, more details on some of the derivations, and more sample problems to ensure that students develop a thorough understanding of the principles.

About the Author:

C. T. SUN, PHD, is the Neil A. Armstrong Distinguished Professor inthe School of Aeronautics and Astronautics at Purdue University in West Lafayette, Indiana, and the recipient of the 2004 Purdue University Research Award. Dr. Sun teaches composites, elasticity, fracture mechanics, and aircraft structures. He is a Fellow of both the American Institute of Aeronautics and Astronautics (AIAA), the American Society of Mechanical Engineers (ASME), and the American Society for Composites (ASC).

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ISBN 10: 0471699667 ISBN 13: 9780471699668
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Descripción John Wiley & Sons, Incorporated, 2006. Estado de conservación: New. 2nd Edition. 2nd Edition-Inventory is subject to prior sale. SHIPPING: Only Standard shipping to PO Boxes. We are not able to ship to APO/FPOs or Internationally. Orders are shipped from Illinois. Nº de ref. de la librería 5200490N1

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Descripción Wiley, 2006. Estado de conservación: New. Brand New, Unread Copy in Perfect Condition. A+ Customer Service! Summary: Preface.Preface to the First Edition.1 Characteristics of Aircraft Structures and Materials.1.1 Introduction.1.2 Basic Structural Elements in Aircraft Structure.1.2.1 Axial Member.1.2.2 Shear Panel.1.2.3 Bending Member (Beam).1.2.4 Torsion Member.1.3 Wing and Fuselage.1.3.1 Load Transfer.1.3.2 Wing Structure.1.3.3 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.2.8.1 Strains Induced by Normal Stress.2.8.2 Strains Induced by Shear Stress.2.8.3 Three-Dimensional Stress-Strain Relations.2.9 Elastic Strain Energy.2.10 Plane Elasticity.2.10.1 Stress-Strain Relations for Plane Isotropic Solids.2.10.2 Stress-Strain Relations for Orthotropic Solids in Plane Stress.2.10.3 Governing Equations.2.10.4 Solution by Airy Stress Function for Plane Isotropic Solids.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.4.3.1 Narrow Rectangular Cross-Section.4.3.2 General Symmetric Sections.4.3.3 Thin-Walled Sections.4.3.4 Shear Deformation in Thin-Walled 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.5.1.1 Symmetric Thin-Walled Sections.5.1.2 Unsymmetric Thin-Walled Sections.5.1.3 Multiple Shear Flow Junctions.5.1.4 Selection of Shear Flow Contour.5.2 Shear Center in Open Sections.5.3 Closed Thin-Walled Sections and Combined Flexural and Torsional Shear Flow.5.3.1 Shear Center.5.3.2 Statically Determinate Shear Flow.5.4 Closed Multicell Sections.Problems.6 Failure Criteria for Isotropic Materials.6.1 Strength Criteria for Brittle Materials.6.1.1 Maximum Principal Stress Criterion.6.1.2 Coulomb-Mohr Criterion.6.2 Yield Criteria for Ductile Materials.6.2.1 Maximum Shear Stress Criterion (Tresca Yield Criterion) in Plane Stress.6.2.2 Maximum Distortion Energy Criterion (von Mises Yield Criterion).6.3 Fracture Mechanics.6.3.1 Stress Concentration.6.3.2 Concept of Cracks and Strain Energy Release Rate.6.3.3 Fracture Criterion.6.4 Stress Intensity Factor.6.4.1 Symmetric Loading (Mode I Fracture).6.4.2 Antisymmetric Loading (Mode II Fracture).6.4.3 Relation betweenK andG.6.4.4 Mixed Mode Fracture.6.5 Effect of Crack Tip Plasticity.6.6 Fatigue Failure.6.6.1 Constant Stress Amplitude.6.6.2S-N Curves.6.6.3 Variable Amplitude Loading.6.7 Fatigue Crack Growth.Problems.7 Elastic Buckling.7.1 Eccentrically Loaded Beam-Column.7.2 Elastic Buckling of Straight Bars.7.2.1 Pinned-Pinned Bar.7.2.2 Clamped-Free Bar.7.2.3 Clamped-Pinned Bar.7.2.4 Clamped-Clamped Bar.7.2.5 Effective Length of Buckling.7.3 Initial Imperfection.7.4 Postbuckling Behavior.7.5 Bar of Unsymmetric Section.7.6 Torsion. Nº de ref. de la librería ABE_book_new_0471699667

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Descripción Wiley, 2006. Hardcover. Estado de conservación: New. book. Nº de ref. de la librería 0471699667

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Descripción John Wiley and Sons Ltd, United States, 2006. Hardback. Estado de conservación: New. 2nd Revised edition. 236 x 160 mm. Language: English . Brand New Book. Designed to help students get a solid background in structural mechanics and extensively updated to help professionals get up to speed on recent advances This Second Edition of the bestselling textbook Mechanics of Aircraft Structures combines fundamentals, an overview of new materials, and rigorous analysis tools into an excellent one-semester introductory course in structural mechanics and aerospace engineering. It s also extremely useful to practicing aerospace or mechanical engineers who want to keep abreast of new materials and recent advances. Updated and expanded, this hands-on reference covers: Introduction to elasticity of anisotropic solids, including mechanics of composite materials and laminated structures Stress analysis of thin-walled structures with end constraints Elastic buckling of beam-column, plates, and thin-walled bars Fracture mechanics as a tool in studying damage tolerance and durability Designed and structured to provide a solid foundation in structural mechanics, Mechanics of Aircraft Structures, Second Edition includes more examples, more details on some of the derivations, and more sample problems to ensure that students develop a thorough understanding of the principles. Nº de ref. de la librería AAH9780471699668

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Sun, C. T.
Editorial: John Wiley and Sons Ltd, United States (2006)
ISBN 10: 0471699667 ISBN 13: 9780471699668
Nuevos Tapa dura Cantidad: 10
Librería
The Book Depository US
(London, Reino Unido)
Valoración
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Descripción John Wiley and Sons Ltd, United States, 2006. Hardback. Estado de conservación: New. 2nd Revised edition. 236 x 160 mm. Language: English . Brand New Book. Designed to help students get a solid background in structural mechanics and extensively updated to help professionals get up to speed on recent advances This Second Edition of the bestselling textbook Mechanics of Aircraft Structures combines fundamentals, an overview of new materials, and rigorous analysis tools into an excellent one-semester introductory course in structural mechanics and aerospace engineering. It s also extremely useful to practicing aerospace or mechanical engineers who want to keep abreast of new materials and recent advances. Updated and expanded, this hands-on reference covers: Introduction to elasticity of anisotropic solids, including mechanics of composite materials and laminated structures Stress analysis of thin-walled structures with end constraints Elastic buckling of beam-column, plates, and thin-walled bars Fracture mechanics as a tool in studying damage tolerance and durability Designed and structured to provide a solid foundation in structural mechanics, Mechanics of Aircraft Structures, Second Edition includes more examples, more details on some of the derivations, and more sample problems to ensure that students develop a thorough understanding of the principles. Nº de ref. de la librería AAH9780471699668

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