01305nam a22002771i 450099100198816970753620030415131553.0030925s1972 be a||||||||||||||||ita b12226099-39ule_instARCHE-027373ExLBiblioteca InterfacoltàitaA.t.i. Arché s.c.r.l. Pandora Sicilia s.r.l.Senelle, Robert128305La revisione della costituzione :1967-1971 /di Robert SenelleBruxelles :[s.n.],1972250 p., [1] c. :ill. ;22 cmTesti e documenti ;73-74-75Sul front.: Ministero degli affari esteri, del commercio con l'estero e della cooperazione allo sviluppoItaliaCostituzioni politiche.b1222609902-04-1408-10-03991001988169707536LE002 St. XIX A 1212002000717047le002-E0.00-l- 00000.i1260827008-10-03LE002 Dir. IV E 2022002000074744le002-E0.00-l- 00000.i1260828208-10-03LE002 Dir. III D 932002000075215le002-E0.00-l- 00000.i1260829408-10-03Revisione della costituzione156142UNISALENTOle00208-10-03ma -itabe 3305357nam 2200673Ia 450 991100474960332120201009050845.097866125417669781282541764128254176597818561793311856179338(CKB)2670000000019545(EBL)648757(SSID)ssj0000420962(PQKBManifestationID)12191681(PQKBTitleCode)TC0000420962(PQKBWorkID)10405587(PQKB)11650695(MiAaPQ)EBC648757(PPN)170266362(FR-PaCSA)88809521(FRCYB88809521)88809521(EXLCZ)99267000000001954520091218d2010 uy 0engur|n|---|||||txtccrIntroduction to aircraft structural analysis /T.H.G. MegsonAmsterdam ;Boston Butterworth-Heinemannc20101 online resource (645 p.)Description based upon print version of record.9781856179324 185617932X Includes bibliographical references and index.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 RELATIONSHIPS1.16 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 WORKChapter 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 SPRING6.3 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 CURVATURE7.6 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 PANELS9.6 FAILURE STRESS IN PLATES AND STIFFENED PANELSBased 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 coreAirframesStructural analysis (Engineering)Airframes.Structural analysis (Engineering)629.134/31629.1341Megson T. H. G(Thomas Henry Gordon)298606Megson T. H. G(Thomas Henry Gordon).298606MiAaPQMiAaPQMiAaPQBOOK9911004749603321Introduction to aircraft structural analysis4392366UNINA