{"product_id":"mechanics-of-aircraft-structures-isbn-9781119583912","title":"Mechanics of Aircraft Structures","description":"MECHANICS OF \u003cb\u003eAIRCRAFT\u003c\/b\u003e STRUCTURES \u003cp\u003e\u003cb\u003eExplore the most up-to-date overview of the foundations of aircraft structures combined with a review of new aircraft materials\u003c\/b\u003e \u003c\/p\u003e\u003cp\u003eThe newly revised Third Edition of \u003ci\u003eMechanics of Aircraft Structures\u003c\/i\u003e delivers a combination of the fundamentals of aircraft structure with an overview of new materials in the industry and a collection of rigorous analysis tools into a single one-stop resource. Perfect for a one-semester introductory course in structural mechanics and aerospace engineering, the distinguished authors have created a textbook that is also ideal for mechanical or aerospace engineers who wish to stay updated on recent advances in the industry. \u003c\/p\u003e\u003cp\u003eThe new edition contains new problems and worked examples in each chapter and improves student accessibility. A new chapter on aircraft loads and new material on elasticity and structural idealization form part of the expanded content in the book. Readers will also benefit from the inclusion of: \u003c\/p\u003e\u003cul\u003e\n\u003cli\u003eA thorough introduction to the characteristics of aircraft structures and materials, including the different types of aircraft structures and their basic structural elements\u003c\/li\u003e \u003cli\u003eAn exploration of load on aircraft structures, including loads on wing, fuselage, landing gear, and stabilizer structures\u003c\/li\u003e \u003cli\u003eAn examination of the concept of elasticity, including the concepts of displacement, strain, and stress, and the equations of equilibrium in a nonuniform stress field\u003c\/li\u003e \u003cli\u003eA treatment of the concept of torsion\u003c\/li\u003e\n\u003c\/ul\u003e \u003cp\u003ePerfect for senior undergraduate and graduate students in aerospace engineering, \u003ci\u003eMechanics of Aircraft Structures\u003c\/i\u003e will also earn a place in the libraries of aerospace engineers seeking a one-stop reference to solidify their understanding of the fundamentals of aircraft structures and discover an overview of new materials in the field. \u003c\/p\u003e\u003cp\u003ePreface to the Third Edition xiii\u003c\/p\u003e \u003cp\u003ePreface to the Second Edition xv\u003c\/p\u003e \u003cp\u003ePreface to the First Edition xvii\u003c\/p\u003e \u003cp\u003eAbout the Companion Website xix\u003c\/p\u003e \u003cp\u003e\u003cb\u003e1 Characteristics of Aircraft Structures and Materials 1\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e1.1 Introduction, 1\u003c\/p\u003e \u003cp\u003e1.2 Types of Aircraft Structures, 1\u003c\/p\u003e \u003cp\u003e1.2.1 Fixed-Wing Aircraft, 2\u003c\/p\u003e \u003cp\u003e1.2.2 Rotorcraft, 2\u003c\/p\u003e \u003cp\u003e1.2.3 Lighter-than-Air Vehicles, 2\u003c\/p\u003e \u003cp\u003e1.2.4 Drones, 2\u003c\/p\u003e \u003cp\u003e1.3 Basic Structural Elements in Aircraft Structure, 3\u003c\/p\u003e \u003cp\u003e1.3.1 Fuselage, 3\u003c\/p\u003e \u003cp\u003e1.3.2 Wing, 3\u003c\/p\u003e \u003cp\u003e1.3.3 Landing Gear, 4\u003c\/p\u003e \u003cp\u003e1.3.4 Control Surfaces, 4\u003c\/p\u003e \u003cp\u003e1.4 Aircraft Materials, 5\u003c\/p\u003e \u003cp\u003e1.4.1 Steel Alloys, 5\u003c\/p\u003e \u003cp\u003e1.4.2 Aluminum Alloys, 6\u003c\/p\u003e \u003cp\u003e1.4.3 Titanium Alloys, 6\u003c\/p\u003e \u003cp\u003e1.4.4 Fiber-Reinforced Composites, 6\u003c\/p\u003e \u003cp\u003eProblems, 7\u003c\/p\u003e \u003cp\u003e\u003cb\u003e2 Loads on Aircraft Structures 9\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e2.1 Introduction, 9\u003c\/p\u003e \u003cp\u003e2.2 Basic Structural Elements, 9\u003c\/p\u003e \u003cp\u003e2.2.1 Axial Member, 9\u003c\/p\u003e \u003cp\u003e2.2.2 Shear Panel, 11\u003c\/p\u003e \u003cp\u003e2.2.3 Bending Member (Beam), 12\u003c\/p\u003e \u003cp\u003e2.2.4 Torsion Member, 13\u003c\/p\u003e \u003cp\u003e2.3 Wing and Fuselage, 15\u003c\/p\u003e \u003cp\u003e2.3.1 Load Transfer, 15\u003c\/p\u003e \u003cp\u003e2.3.2 Wing Structure, 16\u003c\/p\u003e \u003cp\u003e2.3.3 Fuselage, 17\u003c\/p\u003e \u003cp\u003eProblems, 20\u003c\/p\u003e \u003cp\u003e\u003cb\u003e3 Introduction to Elasticity 23\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e3.1 Introduction, 23\u003c\/p\u003e \u003cp\u003e3.2 Concept of Displacement, 24\u003c\/p\u003e \u003cp\u003e3.3 Strain, 26\u003c\/p\u003e \u003cp\u003e3.3.1 Rigid Body Motion, 28\u003c\/p\u003e \u003cp\u003e3.4 Stress, 30\u003c\/p\u003e \u003cp\u003e3.5 Equations of Equilibrium in a Uniform Stress Field, 31\u003c\/p\u003e \u003cp\u003e3.6 Equations of Equilibrium in a Nonuniform Stress Field, 33\u003c\/p\u003e \u003cp\u003e3.7 Stress Vector and Stress Components Relations, 35\u003c\/p\u003e \u003cp\u003e3.8 Principal Stress, 37\u003c\/p\u003e \u003cp\u003e3.9 Shear Stress, 40\u003c\/p\u003e \u003cp\u003e3.10 Stress Transformation, 41\u003c\/p\u003e \u003cp\u003e3.11 Linear Stress–Strain Relations, 44\u003c\/p\u003e \u003cp\u003e3.11.1 Strains Induced by Normal Stress, 45\u003c\/p\u003e \u003cp\u003e3.11.2 Strains Induced by Shear Stress, 47\u003c\/p\u003e \u003cp\u003e3.11.3 Three-Dimensional Stress–Strain Relations, 47\u003c\/p\u003e \u003cp\u003e3.11.3.1 Orthotropic Materials, 49\u003c\/p\u003e \u003cp\u003e3.11.3.2 Isotropic Materials, 50\u003c\/p\u003e \u003cp\u003e3.12 Plane Elasticity, 51\u003c\/p\u003e \u003cp\u003e3.12.1 Stress–Strain Relations for Plane Isotropic Solids, 52\u003c\/p\u003e \u003cp\u003e3.12.1.1 Plane Strain, 52\u003c\/p\u003e \u003cp\u003e3.12.1.2 Plane Stress, 53\u003c\/p\u003e \u003cp\u003e3.12.2 Stress–Strain Relations for Orthotropic Solids in Plane Stress, 54\u003c\/p\u003e \u003cp\u003e3.12.3 Governing Equations, 55\u003c\/p\u003e \u003cp\u003e3.12.3.1 Equilibrium Equations, 55\u003c\/p\u003e \u003cp\u003e3.12.3.2 Boundary Conditions, 55\u003c\/p\u003e \u003cp\u003e3.12.3.3 Compatibility Equation, 56\u003c\/p\u003e \u003cp\u003e3.12.4 Solution by Airy Stress Function for Plane Isotropic Solids, 57\u003c\/p\u003e \u003cp\u003e3.12.5 Plane Elasticity Solutions in Polar Coordinate System, 59\u003c\/p\u003e \u003cp\u003e3.12.5.1 Strain–Displacement Relations, 59\u003c\/p\u003e \u003cp\u003e3.12.5.2 Stresses in Polar Coordinates and Equilibrium Equations, 60\u003c\/p\u003e \u003cp\u003e3.12.5.3 Stress–Strain Relations, 61\u003c\/p\u003e \u003cp\u003e3.12.5.4 Stress Function Formulations, 61\u003c\/p\u003e \u003cp\u003e3.13 Formulations Beyond 2-D Plane Elasticity, 62\u003c\/p\u003e \u003cp\u003eProblems, 64\u003c\/p\u003e \u003cp\u003eReferences, 71\u003c\/p\u003e \u003cp\u003e\u003cb\u003e4 Torsion 73\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e4.1 Introduction, 73\u003c\/p\u003e \u003cp\u003e4.2 Torsion of Uniform Bars With Arbitrary Cross-Section, 73\u003c\/p\u003e \u003cp\u003e4.2.1 Governing Equations, 74\u003c\/p\u003e \u003cp\u003e4.2.2 Boundary Conditions, 76\u003c\/p\u003e \u003cp\u003e4.2.3 Torque–Stress Relations, 77\u003c\/p\u003e \u003cp\u003e4.2.4 Warping Displacement, 78\u003c\/p\u003e \u003cp\u003e4.2.5 Torsion Constant, 79\u003c\/p\u003e \u003cp\u003e4.3 Bars With Circular Cross-Sections, 79\u003c\/p\u003e \u003cp\u003e4.3.1 Elasticity Approach Using Prandtl Stress Function, 79\u003c\/p\u003e \u003cp\u003e4.3.2 Mechanics of Solid Approach, 82\u003c\/p\u003e \u003cp\u003e4.4 Bars With Narrow Rectangular Cross-Sections, 85\u003c\/p\u003e \u003cp\u003e4.5 Closed Single-Cell Thin-Walled Sections, 88\u003c\/p\u003e \u003cp\u003e4.5.1 The s–n Coordinate System, 88\u003c\/p\u003e \u003cp\u003e4.5.2 Prandtl Stress Function, 90\u003c\/p\u003e \u003cp\u003e4.5.3 Shear Flow q, 91\u003c\/p\u003e \u003cp\u003e4.5.4 Shear Flow–Torque Relation, 91\u003c\/p\u003e \u003cp\u003e4.5.5 Twist Angle, 93\u003c\/p\u003e \u003cp\u003e4.5.5.1 Method 1, 93\u003c\/p\u003e \u003cp\u003e4.5.5.2 Method 2 for Constant Shear Flow, 94\u003c\/p\u003e \u003cp\u003e4.5.6 Torsion Constant J, 95\u003c\/p\u003e \u003cp\u003e4.6 Multicell Thin-Walled Sections, 98\u003c\/p\u003e \u003cp\u003e4.7 Warping in Open Thin-Walled Sections, 102\u003c\/p\u003e \u003cp\u003e4.8 Warping in Closed Thin-Walled Sections, 106\u003c\/p\u003e \u003cp\u003e4.9 Effect of End Constraints, 108\u003c\/p\u003e \u003cp\u003eProblems, 114\u003c\/p\u003e \u003cp\u003eReferences, 119\u003c\/p\u003e \u003cp\u003e\u003cb\u003e5 Bending and Flexural Shear 121\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e5.1 Introduction, 121\u003c\/p\u003e \u003cp\u003e5.2 Bernoulli–Euler Beam Theory, 121\u003c\/p\u003e \u003cp\u003e5.2.1 Unidirectional Bending on Beams with a Symmetric Section, 121\u003c\/p\u003e \u003cp\u003e5.2.2 Bidirectional Bending on Beams with an Arbitrary Section, 127\u003c\/p\u003e \u003cp\u003e5.3 Structural Idealization, 131\u003c\/p\u003e \u003cp\u003e5.4 Transverse Shear Stress Due to Transverse Force in Symmetric Sections, 139\u003c\/p\u003e \u003cp\u003e5.4.1 Narrow Rectangular Cross-Section, 139\u003c\/p\u003e \u003cp\u003e5.4.2 General Symmetric Sections, 141\u003c\/p\u003e \u003cp\u003e5.4.3 Thin-Walled Sections, 142\u003c\/p\u003e \u003cp\u003e5.4.4 Shear Deformation in Thin-Walled Sections, 143\u003c\/p\u003e \u003cp\u003e5.5 Timoshenko Beam Theory, 146\u003c\/p\u003e \u003cp\u003e5.6 Saint-Venant’s principle, 149\u003c\/p\u003e \u003cp\u003e5.7 Shear Lag, 152\u003c\/p\u003e \u003cp\u003eProblems, 155\u003c\/p\u003e \u003cp\u003eReference, 160\u003c\/p\u003e \u003cp\u003e\u003cb\u003e6 Flexural Shear Flow in Thin-Walled Sections 161\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e6.1 Introduction, 161\u003c\/p\u003e \u003cp\u003e6.2 Flexural Shear Flow in Open Thin-Walled Sections, 161\u003c\/p\u003e \u003cp\u003e6.2.1 Symmetric Thin-Walled Sections, 161\u003c\/p\u003e \u003cp\u003e6.2.1.1 Stringer–Web Sections, 164\u003c\/p\u003e \u003cp\u003e6.2.2 Unsymmetric Thin-Walled Sections, 166\u003c\/p\u003e \u003cp\u003e6.2.3 Multiple Shear Flow Junctions, 168\u003c\/p\u003e \u003cp\u003e6.2.4 Selection of Shear Flow Contour, 169\u003c\/p\u003e \u003cp\u003e6.3 Shear Center in Open Sections, 169\u003c\/p\u003e \u003cp\u003e6.4 Closed Thin-Walled Sections and Combined Flexural and Torsional Shear Flow, 175\u003c\/p\u003e \u003cp\u003e6.4.1 Shear Center, 176\u003c\/p\u003e \u003cp\u003e6.4.2 Statically Determinate Shear Flow, 179\u003c\/p\u003e \u003cp\u003e6.5 Closed Multicell Sections, 182\u003c\/p\u003e \u003cp\u003eProblems, 186\u003c\/p\u003e \u003cp\u003e\u003cb\u003e7 Failure Criteria for Isotropic Materials 193\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e7.1 Introduction, 193\u003c\/p\u003e \u003cp\u003e7.2 Strength Criteria for Brittle Materials, 193\u003c\/p\u003e \u003cp\u003e7.2.1 Maximum Principal Stress Criterion, 193\u003c\/p\u003e \u003cp\u003e7.2.2 Coulomb–Mohr Criterion, 194\u003c\/p\u003e \u003cp\u003e7.3 Yield Criteria for Ductile Materials, 196\u003c\/p\u003e \u003cp\u003e7.3.1 Maximum Shear Stress Criterion (Tresca Yield Criterion) in Plane Stress, 196\u003c\/p\u003e \u003cp\u003e7.3.2 Maximum Distortion Energy Criterion (von Mises Yield Criterion), 197\u003c\/p\u003e \u003cp\u003e7.4 Fracture Mechanics, 203\u003c\/p\u003e \u003cp\u003e7.4.1 Stress Concentration, 203\u003c\/p\u003e \u003cp\u003e7.4.2 Concept of Cracks and Strain Energy Release Rate, 204\u003c\/p\u003e \u003cp\u003e7.4.3 Fracture Criterion, 205\u003c\/p\u003e \u003cp\u003e7.4.3.1 Strain Energy in Structural Members, 205\u003c\/p\u003e \u003cp\u003e7.4.3.2 Axial Element, 206\u003c\/p\u003e \u003cp\u003e7.4.3.3 Beam Element, 206\u003c\/p\u003e \u003cp\u003e7.4.3.4 Torsion Member, 206\u003c\/p\u003e \u003cp\u003e7.5 Stress Intensity Factor, 210\u003c\/p\u003e \u003cp\u003e7.5.1 Symmetric Loading (Mode I Fracture), 210\u003c\/p\u003e \u003cp\u003e7.5.2 Antisymmetric Loading (Mode II Fracture), 212\u003c\/p\u003e \u003cp\u003e7.5.3 Relation between K and G, 213\u003c\/p\u003e \u003cp\u003e7.5.4 Mixed Mode Fracture, 217\u003c\/p\u003e \u003cp\u003e7.6 Effect of Crack Tip Plasticity, 218\u003c\/p\u003e \u003cp\u003e7.7 Fatigue Failure, 220\u003c\/p\u003e \u003cp\u003e7.7.1 Constant Stress Amplitude, 220\u003c\/p\u003e \u003cp\u003e7.7.2 S–N Curves, 221\u003c\/p\u003e \u003cp\u003e7.7.3 Variable Amplitude Loading, 221\u003c\/p\u003e \u003cp\u003e7.8 Fatigue Crack Growth, 222\u003c\/p\u003e \u003cp\u003eProblems, 224\u003c\/p\u003e \u003cp\u003eReferences, 228\u003c\/p\u003e \u003cp\u003e\u003cb\u003e8 Elastic Buckling 229\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e8.1 Introduction, 229\u003c\/p\u003e \u003cp\u003e8.2 Eccentrically Loaded Beam-Column, 229\u003c\/p\u003e \u003cp\u003e8.3 Elastic Buckling of Straight Bars, 230\u003c\/p\u003e \u003cp\u003e8.3.1 Pinned–Pinned Bar, 232\u003c\/p\u003e \u003cp\u003e8.3.2 Clamped–Free Bar, 235\u003c\/p\u003e \u003cp\u003e8.3.3 Clamped–Pinned Bar, 236\u003c\/p\u003e \u003cp\u003e8.3.4 Clamped–Clamped Bar, 237\u003c\/p\u003e \u003cp\u003e8.3.5 Effective Length of Buckling, 238\u003c\/p\u003e \u003cp\u003e8.4 Initial Imperfection, 239\u003c\/p\u003e \u003cp\u003e8.5 Postbuckling Behavior, 241\u003c\/p\u003e \u003cp\u003e8.6 Bar of Unsymmetric Section, 246\u003c\/p\u003e \u003cp\u003e8.7 Torsional–Flexural Buckling of Thin-Walled Bars, 248\u003c\/p\u003e \u003cp\u003e8.7.1 Nonuniform Torsion, 248\u003c\/p\u003e \u003cp\u003e8.7.2 Torsional Buckling of Doubly Symmetric Section, 249\u003c\/p\u003e \u003cp\u003e8.7.3 Torsional–Flexural Buckling, 252\u003c\/p\u003e \u003cp\u003e8.8 Elastic Buckling of Flat Plates, 256\u003c\/p\u003e \u003cp\u003e8.8.1 Governing Equation for Flat Plates, 256\u003c\/p\u003e \u003cp\u003e8.8.1.1 Boundary Conditions, 257\u003c\/p\u003e \u003cp\u003e8.8.1.2 Clamped Edge, 258\u003c\/p\u003e \u003cp\u003e8.8.1.3 Simply Supported Edge, 258\u003c\/p\u003e \u003cp\u003e8.8.1.4 Free Edge, 258\u003c\/p\u003e \u003cp\u003e8.8.2 Cylindrical Bending, 258\u003c\/p\u003e \u003cp\u003e8.8.3 Buckling of Rectangular Plates, 259\u003c\/p\u003e \u003cp\u003e8.8.3.1 Simply Supported Edges, 259\u003c\/p\u003e \u003cp\u003e8.8.3.2 Other Boundary Conditions, 262\u003c\/p\u003e \u003cp\u003e8.8.4 Buckling Under Shearing Stresses, 262\u003c\/p\u003e \u003cp\u003e8.9 Local Buckling of Open Sections, 263\u003c\/p\u003e \u003cp\u003eProblems, 265\u003c\/p\u003e \u003cp\u003e\u003cb\u003e9 Analysis of Composite Laminates 271\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003e9.1 Plane Stress Equations for Composite Lamina, 271\u003c\/p\u003e \u003cp\u003e9.2 Off-Axis Loading, 276\u003c\/p\u003e \u003cp\u003e9.3 Notation for Stacking Sequence in Laminates, 278\u003c\/p\u003e \u003cp\u003e9.3.1 Symmetry, 279\u003c\/p\u003e \u003cp\u003e9.3.2 Repetition, 279\u003c\/p\u003e \u003cp\u003e9.4 Symmetric Laminate Under In-Plane Loading, 279\u003c\/p\u003e \u003cp\u003e9.5 Effective Moduli for Symmetric Laminates, 281\u003c\/p\u003e \u003cp\u003e9.5.1 Quasi-Isotropic Laminate, 283\u003c\/p\u003e \u003cp\u003e9.6 Laminar Stresses, 284\u003c\/p\u003e \u003cp\u003e9.7 [±45 ] Laminate, 286\u003c\/p\u003e \u003cp\u003e9.7.1 Determination of G 12 Using ±45 Laminates, 287\u003c\/p\u003e \u003cp\u003eProblems, 288\u003c\/p\u003e \u003cp\u003eIndex 291\u003c\/p\u003e \u003cp\u003e\u003cb\u003eC. T. Sun, PhD,\u003c\/b\u003e is Neil A. Armstrong Distinguished Professor Emeritus of Aeronautics and Astronautics at Purdue University. Dr. Sun was the inaugural recipient of the AIAA-ASC James H. Starnes Award and the 2007 ASME Warner T. Koiter Medal.\u003c\/p\u003e \u003cp\u003e\u003cb\u003eAshfaq Adnan, PhD,\u003c\/b\u003e is Professor in the Mechanical and Aerospace Engineering Department at the University of Texas at Arlington and a Fellow of ASME. His research focus is on deformation, damage, and failure of biological, bioinspired, and engineered materials at multiple length scales.  \u003c\/p\u003e\u003cp\u003e\u003cb\u003eExplore the most up-to-date overview of the foundations of aircraft structures combined with a review of new aircraft materials\u003c\/b\u003e\u003c\/p\u003e \u003cp\u003eThe newly revised Third Edition of \u003ci\u003eMechanics of Aircraft Structures\u003c\/i\u003e delivers a combination of the fundamentals of aircraft structure with an overview of new materials in the industry and a collection of rigorous analysis tools into a single one-stop resource. Perfect for a one-semester introductory course in structural mechanics and aerospace engineering, the distinguished authors have created a textbook that is also ideal for mechanical or aerospace engineers who wish to stay updated on recent advances in the industry. \u003c\/p\u003e\u003cp\u003eThe new edition contains new problems and worked examples in each chapter and improves student accessibility. A new chapter on aircraft loads and new material on elasticity and structural idealization form part of the expanded content in the book. Readers will also benefit from the inclusion of: \u003c\/p\u003e\u003cul\u003e\n\u003cli\u003eA thorough introduction to the characteristics of aircraft structures and materials, including the different types of aircraft structures and their basic structural elements\u003c\/li\u003e \u003cli\u003eAn exploration of load on aircraft structures, including loads on wing, fuselage, landing gear, and stabilizer structures\u003c\/li\u003e \u003cli\u003eAn examination of the concept of elasticity, including the concepts of displacement, strain, and stress, and the equations of equilibrium in a nonuniform stress field\u003c\/li\u003e \u003cli\u003eA treatment of the concept of torsion\u003c\/li\u003e\n\u003c\/ul\u003e \u003cp\u003ePerfect for senior undergraduate and graduate students in aerospace engineering, \u003ci\u003eMechanics of Aircraft Structures\u003c\/i\u003e will also earn a place in the libraries of aerospace engineers seeking a one-stop reference to solidify their understanding of the fundamentals of aircraft structures and discover an overview of new materials in the field.\u003c\/p\u003e","brand":"Wiley","offers":[{"title":"Default Title","offer_id":47989596258533,"sku":"NP9781119583912","price":128.0,"currency_code":"USD","in_stock":false}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/1842\/7735\/files\/9781119583912.jpg?v=1761784744","url":"https:\/\/k12savings.com\/products\/mechanics-of-aircraft-structures-isbn-9781119583912","provider":"K12savings","version":"1.0","type":"link"}