LEADER 03832nam 2200481za 450 001 9911007031803321 005 20250423122449.0 010 $a9780323902113 010 $a0323902111 010 $a9780128228685 010 $a0128228687 035 $a(CKB)5600000000002643 035 $a(NjHacI)995600000000002643 035 $a(PPN)263623696 035 $a(FR-PaCSA)88930519 035 $a(FRCYB88930519)88930519 035 $a(EXLCZ)995600000000002643 100 $a20220913d2022 uy 0 101 0 $aeng 135 $aur|n|nnn||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aAircraft structures for engineering students /$fT.H.G. Megson 205 $a7th ed. 210 $aOxford $cButterworth-Heinemann$d2022 215 $a1 online resource (xv, 944 p.) $cill 225 1 $aElsevier aerospace engineering series 327 $aPart A: Fundamentals of Structural Analysis -- Section A1: Elasticity -- 1. Basic elasticity -- 2. Two-dimensional problems in elasticity -- 3. Torsion of solid sections -- Section A2: Virtual work, energy, and matrix methods -- 4. Virtual work and energy methods -- 5. Energy methods -- 6. Matrix methods Section -- A3: Thin plate theory -- 7. Bending of thin plates -- Section A4: Structural instability -- 8. Columns -- 9. Thin plates -- Section A5: Vibration of structures -- 10. Structural vibration -- Part B: Analysis of Aircraft Structures Section -- B1: Principles of stressed skin construction -- 11. Materials -- 12. Structural components of aircraft -- Section B2: Airworthiness and airframe loads -- 13. Airworthiness -- 14. Airframe loads -- 15. Fatigue -- Section B3: Bending, shear and torsion of thin-walled beams -- 16. Bending of open and closed, thin-walled beams -- 17. Shear of beams -- 18. Torsion of beams -- 19. Combined open and closed section beams -- 20. Structural idealization -- Section B4: Stress analysis of aircraft components -- 21. Wing spars and box beams -- 22. Fuselages -- 23. Wings -- 24. Fuselage frames and wing ribs -- 25. Laminated composite structures -- Section B5: Structural and loading discontinuities -- 26. Closed section beams -- 27. Open section beams -- Section B6: Introduction to aeroelasticity -- 28. Wing problems -- Appendix: Design of a rear fuselage -- Index. 330 $aAircraft Structures for Engineering Students, seventh edition, is the leading self-contained aircraft structures course text suitable for one or more semesters. It covers all fundamental subjects, including elasticity, structural analysis, airworthiness and aeroelasticity. Now in its seventh edition, the author has continued to expand the book?s coverage of analysis and design of composite materials for use in aircraft and has added more real-world and design-based examples, along with new end-of-chapter problems of varying complexity. Retains its hallmark comprehensive coverage of aircraft structural analysis; New practical and design-based examples and problems throughout the text aid understanding and relate concepts to real world applications; Updated and additional Matlab examples and exercises support use of computational tools in analysis and design; Available online teaching and learning tools include downloadable Matlab code, solutions manual, and image bank of figures from the book. 410 0$aElsevier aerospace engineering series. 606 $aAirframes 606 $aStructural analysis (Engineering) 615 0$aAirframes. 615 0$aStructural analysis (Engineering) 676 $a629.13431 700 $aMegson$b T. H. G$g(Thomas Henry Gordon)$0298606 801 0$bNjHacI 801 1$bNjHacl 906 $aBOOK 912 $a9911007031803321 996 $aAircraft structures for engineering students$9726330 997 $aUNINA