Introduction to Aircraft Structural Analysis
Autor T. H. G. Megsonen Limba Engleză Paperback – 14 iun 2017
- Based on the author's best-selling text, Aircraft Structures for Engineering Students
- Contains expanded coverage of composite materials and structures<
- Includes new practical and design-based examples and problems throughout the text
- Provides an online teaching and learning tool with downloadable MATLAB code, a solutions manual, and an image bank of figures from the book
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Specificații
ISBN-13: 9780081020760
ISBN-10: 0081020767
Pagini: 758
Dimensiuni: 191 x 235 x 43 mm
Greutate: 1.53 kg
Ediția:3
Editura: ELSEVIER SCIENCE
ISBN-10: 0081020767
Pagini: 758
Dimensiuni: 191 x 235 x 43 mm
Greutate: 1.53 kg
Ediția:3
Editura: ELSEVIER SCIENCE
Public țintă
Undergraduate and postgraduate students of aerospace and aeronautical engineering. Also suitable for professional development and training coursesCuprins
1. Basic elasticity
2. Two-dimensional problems in elasticity
3. Torsion of solid sections
4. Virtual work and energy methods
5. Energy methods
6. Matrix methods
7. Bending of thin plates
8. Columns
9. Thin plates
10. Materials
11. Structural components of aircraft
12. Airworthiness
13. Airframe loads
14. Fatigue
15. Bending of open and closed thin-walled beams
16. Shear of beams
17. Torsion of beams
18. Combined open and closed section beams
19. Structural idealization
20. Wing spars and box beams
21. Fuselages
22. Wings
23. Fuselage frames and wing ribs
24. Laminated composite structures
2. Two-dimensional problems in elasticity
3. Torsion of solid sections
4. Virtual work and energy methods
5. Energy methods
6. Matrix methods
7. Bending of thin plates
8. Columns
9. Thin plates
10. Materials
11. Structural components of aircraft
12. Airworthiness
13. Airframe loads
14. Fatigue
15. Bending of open and closed thin-walled beams
16. Shear of beams
17. Torsion of beams
18. Combined open and closed section beams
19. Structural idealization
20. Wing spars and box beams
21. Fuselages
22. Wings
23. Fuselage frames and wing ribs
24. Laminated composite structures