Introduction to Aircraft Structural Analysis (3rd Ed.)
Auteur : Megson T.H.G.
Introduction to Aircraft Structure Analysis, Third Edition 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. As a self-contained guide, this value-priced book is an excellent resource for anyone learning the subject.
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
Undergraduate and postgraduate students of aerospace and aeronautical engineering. Also suitable for professional development and training courses
- 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
Date de parution : 06-2017
Ouvrage de 758 p.
19x23.3 cm
Thème d’Introduction to Aircraft Structural Analysis :
Mots-clés :
Aileron effectiveness; bending displacements; Buckling coefficients; Closed section beams; Composite thin-walled beams; Constant shear flow; Control surface flutter; Crack propagation; Crack tip plasticity; Critical stress; Deflections; Distributed torque; Euler theory; Fatigue life; Flexural-torsional buckling; Fuselage frames; Gust loads; In plane loads; Inelastic buckling; landing loads; Load intensity; Mohr’s circle; Multicell wings; Prandtl stress function solution; Propagation rates; Rate of twist; Reciprocal theorem; Rectangular section box; shear; Shear flow; shear force; Shear lag; Singularity functions; Space frames; St Venant warping function solution; St Venant’s principle; Stiffness matrices; Strain energy; Stress-strain relationships; Stringer sections; Symmetric maneuver loads; Tension field beams; Three-boom shell; Torsional divergence; Unit load method; Variable stringer areas; Warping