MARC Record from marc_columbia

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035 $a(NNC)12871887
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049 $aZCUA
100 1 $aMegson, T. H. G.$q(Thomas Henry Gordon)
245 13 $aAn introduction to aircraft structural analysis /$cT.H.G. Megson.
264 1 $aAmsterdam ;$aBoston :$bButterworth-Heinemann/Elsevier,$c2010.
264 4 $c©2010
300 $a1 online resource (vii, 638 pages) :$billustrations
336 $atext$btxt$2rdacontent
337 $acomputer$bc$2rdamedia
338 $aonline resource$bcr$2rdacarrier
500 $aRevised edition of: Aircraft structures for engineering students / T.H.G. Megson. 4th ed. 2007.
504 $aIncludes bibliographical references and index.
520 $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 concepts in about 200 fewer pages by removing some optional topics like structural vibrations and aero elasticity Systematic step by step procedures in the worked examples Self-contained, with complete derivations for key equations Based on the author's best-selling text Aircraft Structures for Engineering Students, this Intro version covers the core concepts in about 200 fewer pages by removing some optional topics like structural vibrations and aeroelasticity Systematic step by step procedures in the worked examples Self-contained, with complete derivations for key equations.
588 0 $aPrint version record.
505 0 $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.
505 8 $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.
505 8 $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.
505 8 $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.
505 8 $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.
650 0 $aAirframes.
650 0 $aStructural analysis (Engineering)
650 7 $aTRANSPORTATION$xAviation$xGeneral.$2bisacsh
650 7 $aAirframes.$2fast$0(OCoLC)fst00802910
650 7 $aStructural analysis (Engineering)$2fast$0(OCoLC)fst01135602
650 4 $aEngineering.
655 0 $aElectronic books.
655 0 $aElectronic book.
655 4 $aElectronic books.
700 1 $aMegson, T. H. G.$q(Thomas Henry Gordon).$tAircraft structures for engineering students.
776 08 $iPrint version:$aMegson, T.H.G. (Thomas Henry Gordon).$tIntroduction to aircraft structural analysis.$dAmsterdam ; Boston : Butterworth-Heinemann/Elsevier, ©2010$w(DLC) 2009050354$w(OCoLC)490807676
856 40 $uhttp://www.columbia.edu/cgi-bin/cul/resolve?clio12871887.001$zACADEMIC - Aerospace & Radar Technology
856 40 $uhttp://www.columbia.edu/cgi-bin/cul/resolve?clio12871887.002$zACADEMIC - Mechanics & Mechanical Engineering
852 8 $blweb$hEBOOKS