LEADER 01877oam 2200493M 450 001 9910716415703321 005 20200213070554.6 035 $a(CKB)5470000002521992 035 $a(OCoLC)1065898786 035 $a(OCoLC)995470000002521992 035 $a(EXLCZ)995470000002521992 100 $a20071213d1926 ua 0 101 0 $aeng 135 $aurcn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aTransient second-class mail matter. December 8, 1926. -- Committed to the Committee of the Whole House on the State of the Union and ordered to be printed 210 1$a[Washington, D.C.] :$c[U.S. Government Printing Office],$d1926. 215 $a1 online resource (1 page) 225 1 $aHouse report / 69th Congress, 2nd session. House ;$vno. 1613 225 1 $a[United States congressional serial set] ;$v[serial no. 8688] 300 $aBatch processed record: Metadata reviewed, not verified. Some fields updated by batch processes. 300 $aFDLP item number not assigned. 606 $aPostal service$xLaw and legislation 606 $aPostal rates 606 $aRevenue 606 $aPostal service 606 $aPostal service$xSecond-class matter 608 $aLegislative materials.$2lcgft 615 0$aPostal service$xLaw and legislation. 615 0$aPostal rates. 615 0$aRevenue. 615 0$aPostal service. 615 0$aPostal service$xSecond-class matter. 701 $aKelly$b Clyde$f1883-1935$pProgressive (PA)$01401903 801 0$bWYU 801 1$bWYU 801 2$bOCLCO 801 2$bOCLCQ 906 $aBOOK 912 $a9910716415703321 996 $aTransient second-class mail matter. December 8, 1926. -- Committed to the Committee of the Whole House on the State of the Union and ordered to be printed$93471275 997 $aUNINA LEADER 05195nam 2200589 a 450 001 9911007084103321 005 20200520144314.0 010 $a0-08-096906-2 035 $a(CKB)2670000000154968 035 $a(EBL)862036 035 $a(OCoLC)778339796 035 $a(SSID)ssj0000631798 035 $a(PQKBManifestationID)11941466 035 $a(PQKBTitleCode)TC0000631798 035 $a(PQKBWorkID)10599993 035 $a(PQKB)10687945 035 $a(MiAaPQ)EBC862036 035 $a(EXLCZ)992670000000154968 100 $a20130820d2013 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 10$aAircraft structures for engineering students /$fT. H. G. Megson 205 $a5th ed. 210 $aOxford, England ;$aWaltham, Mass. $cButterworth-Heinemann$dc2013 215 $a1 online resource (875 p.) 225 0$aElsevier aerospace engineering series 300 $aDescription based upon print version of record. 311 $a0-08-096905-4 320 $aIncludes bibliographical references at the end of each chapters and index. 327 $aFront Cover; Aircraft Structures for engineering students; Copyright; Dedication; Contents; Preface; Part A: Fundamentals of structural analysis; Section A1: Elasticity; Chapter 1: 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 327 $aExperimental measurement of surface strainsReferences; Additional Reading; Chapter 2: 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 sections; Prandtl stress function solution; St. Venant warping function solution; The membrane analogy; Torsion of a narrow rectangular strip; References; Section A2: Virtual work, energy, and matrix methods; Chapter 4: Virtual work and energy methods; Work 327 $aPrinciple of virtual workPrinciple 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; Strain energy and complementary energy; Principle of the stationary value of the total complementary energy; Application to deflection problems 327 $aApplication to the solution of statically indeterminate systemsUnit 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; 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 327 $aStiffness matrix for a uniform beamFinite 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; Section A3: Thin plate theory; Chapter 7: 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 327 $aBending of thin plates having a small initial curvature 330 $aAircraft Structures for Engineering Students is the leading self contained aircraft structures course text. It covers all fundamental subjects, including elasticity, structural analysis, airworthiness and aeroelasticity. Now in its fifth edition, the author has revised and updated the text throughout and added new examples and exercises using Matlab(c). Additional worked examples make the text even more accessible by showing application of concepts to airframe structures. Includes a Solutions Manual available to all adopting teachers. * New worked examples throughout the tex 606 $aAirframes$vTextbooks 606 $aStructural analysis (Engineering)$vTextbooks 615 0$aAirframes 615 0$aStructural analysis (Engineering) 676 $a629.134/31 700 $aMegson$b T. H. G$g(Thomas Henry Gordon)$0298606 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9911007084103321 996 $aAircraft structures for engineering students$9726330 997 $aUNINA