Introduction to aircraft structural analysis / / T.H.G. Megson

• Autore: Megson T. H. G (Thomas Henry Gordon)
• Pubblicazione: Amsterdam ; ; Boston, : Butterworth-Heinemann, c2010
• Descrizione fisica: 1 online resource (645 p.)
• Disciplina: 629.134/31; 629.1341
• Soggetto topico: Airframes; Structural analysis (Engineering)
• Altri autori: MegsonT. H. G (Thomas Henry Gordon)
• Note generali: Description based upon print version of record.
• Nota di bibliografia: Includes bibliographical references and index.
• Nota di contenuto: Front Cover; An Introduction to Aircraft Structural Analysis; Copyright Page; Table of Contents; Preface; 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 STRAINSChapter 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; 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 Methods5.1 STRAIN ENERGY AND COMPLEMENTARY ENERGY; 5.2 THE 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 THE PRINCIPLE OF THE STATIONARY VALUE OF THE TOTAL POTENTIAL ENERGY; 5.9 PRINCIPLE OF SUPERPOSITION; 5.10 THE RECIPROCAL THEOREM; 5.11 TEMPERATURE EFFECTS; Chapter 6. Matrix Methods; 6.1 NOTATION; 6.2 STIFFNESS MATRIX FOR AN ELASTIC SPRING ; 6.3 STIFFNESS MATRIX FOR TWO ELASTIC SPRINGS IN LINE6.4 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; 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 PLATESChapter 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 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
• Sommario/riassunto: 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 set 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. Self-contained, this value-priced book is an excellent resource for anyone learning the subject. Covers the core
• Titolo autorizzato: Introduction to aircraft structural analysis
• ISBN: 9786612541766; 9781282541764; 1282541765; 9781856179331; 1856179338
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9911004749603321
• Lo trovi qui: Univ. Federico II