Notas: | <p><b>Part A: Fundamentals of Structural Analysis </b><i>Section A1: Elasticity </i>1. Basic elasticity 2. Two-dimensional problems in elasticity 3. Torsion of solid sections <i>Section A2: Virtual work, energy, and matrix methods </i>4. Virtual work and energy methods 5. Energy methods 6. Matrix methods <i>Section A3: Thin plate theory </i>7. Bending of thin plates <i>Section A4: Structural instability </i>8. Columns 9. Thin plates <i>Section A5: Vibration of structures </i>10. Structural vibration</p> <p><b>Part B: Analysis of Aircraft Structures </b><i>Section B1: Principles of stressed skin construction </i>11. Materials 12. Structural components of aircraft <i>Section B2: Airworthiness and airframe loads </i>13. Airworthiness 14. Airframe loads 15. Fatigue <i>Section B3: Bending, shear and torsion of thin-walled beams </i>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 <i>Section B4: Stress analysis of aircraft components </i>21. Wing spars and box beams 22. Fuselages 23. Wings 24. Fuselage frames and wing ribs 25. Laminated composite structures <i>Section B5: Structural and loading discontinuities </i>26. Closed section beams 27. Open section beams <i>Section B6: Introduction to aeroelasticity </i>28. Wing problems</p> |