LEADER 05357nam 2200673Ia 450 001 9911004749603321 005 20201009050845.0 010 $a9786612541766 010 $a9781282541764 010 $a1282541765 010 $a9781856179331 010 $a1856179338 035 $a(CKB)2670000000019545 035 $a(EBL)648757 035 $a(SSID)ssj0000420962 035 $a(PQKBManifestationID)12191681 035 $a(PQKBTitleCode)TC0000420962 035 $a(PQKBWorkID)10405587 035 $a(PQKB)11650695 035 $a(MiAaPQ)EBC648757 035 $a(PPN)170266362 035 $a(FR-PaCSA)88809521 035 $a(FRCYB88809521)88809521 035 $a(EXLCZ)992670000000019545 100 $a20091218d2010 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 10$aIntroduction to aircraft structural analysis /$fT.H.G. Megson 210 $aAmsterdam ;$aBoston $cButterworth-Heinemann$dc2010 215 $a1 online resource (645 p.) 300 $aDescription based upon print version of record. 311 08$a9781856179324 311 08$a185617932X 320 $aIncludes bibliographical references and index. 327 $aFront 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 327 $a1.16 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 327 $aChapter 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 327 $a6.3 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 327 $a7.6 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 327 $a9.6 FAILURE STRESS IN PLATES AND STIFFENED PANELS 330 $aBased 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 606 $aAirframes 606 $aStructural analysis (Engineering) 615 0$aAirframes. 615 0$aStructural analysis (Engineering) 676 $a629.134/31 676 $a629.1341 700 $aMegson$b T. H. G$g(Thomas Henry Gordon)$0298606 701 $aMegson$b T. H. G$g(Thomas Henry Gordon).$0298606 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9911004749603321 996 $aIntroduction to aircraft structural analysis$94392366 997 $aUNINA