Aircraft Structures for Engineering Students, 7th Edition
- Length: 960 pages
- Edition: 7
- Language: English
- Publisher: Butterworth-Heinemann
- Publication Date: 2021-09-15
- ISBN-10: 0128228687
- ISBN-13: 9780128228685
- Sales Rank: #848801 (See Top 100 Books)
Aircraft Structures for Engineering Students, Seventh Edition, is the leading self-contained aircraft structures course text suitable for one or more semesters. It covers all fundamental subjects, including elasticity, structural analysis, airworthiness and aeroelasticity. Now in its seventh edition, the author has continued to expand the book’s coverage of analysis and design of composite materials for use in aircraft and has added more real-world and design-based examples, along with new end-of-chapter problems of varying complexity.
Front-Matter_2022_Aircraft-Structures-for-Engineering-Students Front Matter Copyright_2022_Aircraft-Structures-for-Engineering-Students Copyright Dedication_2022_Aircraft-Structures-for-Engineering-Students Dedication Preface-to-the-Seventh-Edition-of-Aircr_2022_Aircraft-Structures-for-Enginee Preface to the Seventh Edition of Aircraft Structures Chapter-1---Basic-elasticity_2022_Aircraft-Structures-for-Engineering-Studen Basic elasticity Stress Notation for forces and stresses Equations of equilibrium Plane stress Boundary conditions Determination of stresses on inclined planes Principal stresses Mohr's circle of stress Strain Compatibility equations Plane strain Determination of strains on inclined planes Principal strains Mohr's circle of strain Stress-strain relationships Temperature effects Experimental measurement of surface strains Reference Further reading Chapter-2---Two-dimensional-problems-i_2022_Aircraft-Structures-for-Engineer Two-dimensional problems in elasticity Two-dimensional problems Stress functions Inverse and semi-inverse methods St. Venant's principle Displacements Bending of an end-loaded cantilever Reference Chapter-3---Torsion-of-solid-sec_2022_Aircraft-Structures-for-Engineering-St Torsion of solid sections Prandtl stress function solution St. Venant warping function solution The membrane analogy Torsion of a narrow rectangular strip References Chapter-4---Virtual-work-and-energy_2022_Aircraft-Structures-for-Engineering Virtual work and energy methods Principle of virtual work Principle of virtual work for a particle Principle of virtual work for a rigid body Virtual work in a deformable body Work done by internal force systems Axial force Shear force Bending moment Torsion Hinges Sign of internal virtual work Virtual work due to external force systems Use of virtual force systems Applications of the principle of virtual work Reference Chapter-5---Energy-methods_2022_Aircraft-Structures-for-Engineering-Students Energy methods Strain energy and complementary energy Principle of the stationary value of the total complementary energy Application to deflection problems Application to the solution of statically indeterminate systems Unit load method Flexibility method Self-straining trusses Total potential energy Principle of the stationary value of the total potential energy Principle of superposition Reciprocal theorem Temperature effects References Further reading Chapter-6---Matrix-methods_2022_Aircraft-Structures-for-Engineering-Students Matrix methods Notation Stiffness matrix for an elastic spring Stiffness matrix for two elastic springs in line Matrix analysis of pin-jointed frameworks Application to statically indeterminate frameworks Matrix analysis of space frames Stiffness matrix for a uniform beam Finite element method for continuum structures Stiffness matrix for a beam-element Stiffness matrix for a triangular finite element Stiffness matrix for a quadrilateral element References Further reading Chapter-7---Bending-of-thin-pla_2022_Aircraft-Structures-for-Engineering-Stu Bending of thin plates Pure bending of thin plates Plates subjected to bending and twisting Plates subjected to a distributed transverse load The simply supported edge The built-in edge The free edge Combined bending and in-plane loading of a thin rectangular plate Bending of thin plates having a small initial curvature Energy method for the bending of thin plates Strain energy produced by bending and twisting Potential energy of a transverse load Potential energy of in-plane loads Further reading Chapter-8---Columns_2022_Aircraft-Structures-for-Engineering-Students Columns Euler buckling of columns Inelastic buckling Effect of initial imperfections Stability of beams under transverse and axial loads Energy method for the calculation of buckling loads in columns Flexural-torsional buckling of thin-walled columns References Chapter-9---Thin-plates_2022_Aircraft-Structures-for-Engineering-Students Thin plates Buckling of thin plates Inelastic buckling of plates Experimental determination of the critical load for a flat plate Local instability Instability of stiffened panels Failure stress in plates and stiffened panels Tension field beams Complete diagonal tension Incomplete diagonal tension Postbuckling behavior References Chapter-10---Structural-vibrat_2022_Aircraft-Structures-for-Engineering-Stud Structural vibration Oscillation of mass-spring systems Oscillation of beams Approximate methods for determining natural frequencies Chapter-11---Materials_2022_Aircraft-Structures-for-Engineering-Students Materials Steel Titanium Polymers Glass Ceramics Composite materials Properties of materials Outline placeholder Ductility Brittleness Elastic materials Plasticity Isotropic materials Anisotropic materials Orthotropic materials Testing of engineering materials Tensile tests Compression tests Bending tests Shear tests Hardness tests Impact tests Stress-strain curves Low carbon steel (mild steel) Aluminum Brittle materials Composites Strain hardening Creep and relaxation Fatigue Chapter-12---Structural-components-of-air_2022_Aircraft-Structures-for-Engin Structural components of aircraft and spacecraft Structural components: Aircraft Loads on structural components Function of structural components Fabrication of structural components Structural components: Spacecraft Outline placeholder Thrust structure Stage structures Adaptors Payload fairings Loads on structural components Connections Riveted connections Simple lap joint Rivet shear Bearing pressure Plate failure in tension Shear failure in a plate Joint efficiency Group-riveted joints Eccentrically loaded riveted joints Welded connections Use of adhesives References Chapter-13---Airworthiness_2022_Aircraft-Structures-for-Engineering-Students Airworthiness Factors of safety: flight envelope Load factor determination Limit load Uncertainties in design and structural deterioration Variation in structural strength Fatigue Airworthiness: Spacecraft Factors of safety Reference Chapter-14---Airframe-loads_2022_Aircraft-Structures-for-Engineering-Student Airframe loads Aircraft inertia loads Symmetric maneuver loads Level flight General case of a symmetric maneuver Normal accelerations associated with various types of maneuver Steady pullout Correctly banked turn Gust loads Sharp-edged gust The graded gust Gust envelope Design loads: Spacecraft References Chapter-15---Fatigue_2022_Aircraft-Structures-for-Engineering-Students Fatigue Safe life and fail-safe structures Designing against fatigue Fatigue strength of components Prediction of aircraft fatigue life Crack propagation Stress concentration factor Crack tip plasticity Crack propagation rates References Further reading Chapter-16---Bending-of-open-and-closed-_2022_Aircraft-Structures-for-Engine Bending of open and closed thin-walled beams Symmetrical bending Assumptions Direct stress distribution Anticlastic bending Unsymmetrical bending Sign conventions and notation Resolution of bending moments Direct stress distribution due to bending Position of the neutral axis Load intensity, shear force, and bending moment relationships, the general case Deflections due to bending Singularity functions Moment-area method for symmetrical bending Calculation of section properties Parallel axes theorem Theorem of perpendicular axes Second moments of area of standard sections Product second moment of area Approximations for thin-walled sections Applicability of bending theory Temperature effects Reference Chapter-17---Shear-of-beams_2022_Aircraft-Structures-for-Engineering-Student Shear of beams General stress, strain, and displacement relationships for open and single-cell closed section thin-walled beams Shear of open section beams Shear center Shear of closed section beams Twist and warping of shear-loaded closed section beams Shear center Reference Chapter-18---Torsion-of-beam_2022_Aircraft-Structures-for-Engineering-Studen Torsion of beams Torsion of closed section beams Displacements associated with the Bredt-Batho shear flow Condition for zero warping at a section Torsion of open section beams Warping of the cross-section Chapter-19---Combined-open-and-closed-_2022_Aircraft-Structures-for-Engineer Combined open and closed section beams Bending Shear Torsion Chapter-20---Structural-idealiza_2022_Aircraft-Structures-for-Engineering-St Structural idealization Principle Idealization of a panel Unsymmetrical sections Effect of idealization on the analysis of open and closed section beams Bending of open and closed section beams Shear of open section beams Shear loading of closed section beams Alternative method for the calculation of shear flow distribution Torsion of open and closed section beams Deflection of open and closed section beams Chapter-21---Wing-spars-and-box-_2022_Aircraft-Structures-for-Engineering-St Wing spars and box beams Open and closed section beams Beams having variable stringer areas Chapter-22---Fuselages_2022_Aircraft-Structures-for-Engineering-Students Fuselages Bending Shear Torsion Pressurized fuselages Cut-outs in fuselages Reference Chapter-23---Wings_2022_Aircraft-Structures-for-Engineering-Students Wings Three-boom shell Bending Torsion Shear Shear center Tapered wings Deflections Cut-outs in wings Chapter-24---Fuselage-frames-and-wi_2022_Aircraft-Structures-for-Engineering Fuselage frames and wing ribs Principles of stiffener/web construction Fuselage frames Wing ribs Chapter-25---Spacecraft_2022_Aircraft-Structures-for-Engineering-Students Spacecraft Natural frequencies Axial stress Stability Reference Chapter-26---Laminated-composite-st_2022_Aircraft-Structures-for-Engineering Laminated composite structures Elastic constants of a simple lamina Stress-strain relationships for an orthotropic ply (macro approach) Specially orthotropic ply Generally orthotropic ply Laminates Assumptions and notation Laminate under in-plane loading Equivalent elastic constants Laminate strengths Thin-walled composite beams Axial load Bending Shear Open section beams Closed section beams Torsion Closed section beams Open section beams Idealization of composite beams References Chapter-27---Closed-section-be_2022_Aircraft-Structures-for-Engineering-Stud Closed section beams General aspects Shear stress distribution at a built-in end of a closed section beam Thin-walled rectangular section beam subjected to torsion Shear lag Reference Chapter-28---Open-section-bea_2022_Aircraft-Structures-for-Engineering-Stude Open section beams I-Section beam subjected to torsion Torsion of an arbitrary section beam Distributed torque loading Extension of the theory to allow for general systems of loading Moment couple (bimoment) Shear flow due to MΓ References Chapter-29---Wing-problems_2022_Aircraft-Structures-for-Engineering-Students Wing problems Load distribution and divergence Wing torsional divergence (two-dimensional case) Wing torsional divergence (finite wing) Swept wing divergence Control effectiveness and reversal Aileron effectiveness and reversal (two-dimensional case) Aileron effectiveness and reversal (finite wing) Introduction to ``flutter´´ Coupling Determination of critical flutter speed Prevention of flutter Experimental determination of flutter speed Control surface flutter References Appendix---Design-of-a-rear-fuse_2022_Aircraft-Structures-for-Engineering-St Appendix: Design of a rear fuselage Specification Data Aircraft Wing Tailplane Fin Initial calculations Flight envelope Fin lift-curve slope Speed of sound Balancing out calculations Case A Fuselage loads Fuselage section Material Self-weight Shear forces and bending moments due to self-weight Total shear forces bending moments and torques Fuselage design calculations Stringer sections Skin thickness Rivet size Skin/stringer rivets Frame/stringer rivets Index_2022_Aircraft-Structures-for-Engineering-Students Index A B C D E F G H I L M N O P Q R S T U V W Y Z
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