Aircraft Structures for Engineering Students (häftad)
Format
Häftad (Paperback)
Språk
Engelska
Antal sidor
910
Utgivningsdatum
2016-11-04
Upplaga
6
Förlag
Butterworth-Heinemann
Illustrationer
Black & white illustrations
Dimensioner
234 x 190 x 57 mm
Vikt
1859 g
Antal komponenter
1
Komponenter
3:B&W 7.5 x 9.25 in or 235 x 191 mm Perfect Bound on White w/Gloss Lam
ISBN
9780081009147
Aircraft Structures for Engineering Students (häftad)

Aircraft Structures for Engineering Students

Häftad Engelska, 2016-11-04
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Aircraft Structures for Engineering Students, Sixth Edition, is the leading self-contained aircraft structures course text. It covers all fundamental subjects, including elasticity, structural analysis, airworthiness and aeroelasticity. Now in its sixth edition, the author has expanded the book's coverage of analysis and design of composite materials for use in aircraft, and has added new, real-world and design-based examples, along with new end-of-chapter problems of varying complexity.

  • Expanded coverage of composite materials and structures
  • 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
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Övrig information

T.H.G. Megson is a professor emeritus with the Department of Civil Engineering at Leeds University (UK). For Elsevier he has written the market leading Butterworth Heinemann textbooks Aircraft Structures for Engineering Students and Introduction to Aircraft Structural Analysis (a briefer derivative of the aircraft structures book), as well as the text/ref hybrid Structural and Stress Analysis.

Innehållsförteckning

Part A: Fundamentals of Structural Analysis Section A1: Elasticity Chapter 1: Basic elasticity Chapter 2: Two-dimensional problems in elasticity Chapter 3: Torsion of solid sections Section A2: Virtual work, energy, and matrix methods Chapter 4: Virtual work and energy methods Chapter 5: Energy methods Chapter 6: Matrix methods Section A3: Thin plate theory Chapter 7: Bending of thin plates Section A4: Structural instability Chapter 8: Columns Chapter 9: Thin plates Section A5: Vibration of structures Chapter 10: Structural vibration Part B: Analysis of Aircraft Structures Section B1: Principles of stressed skin construction Chapter 11: Materials Chapter 12: Structural components of aircraft Section B2: Airworthiness and airframe loads Chapter 13: Airworthiness Chapter 14: Airframe loads Chapter 15: Fatigue Section B3: Bending, shear and torsion of thin-walled beams Chapter 16: Bending of open and closed, thin-walled beams Chapter 17: Shear of beams Chapter 18: Torsion of beams Chapter 19: Combined open and closed section beams Chapter 20: Structural idealization Section B4: Stress analysis of aircraft components Chapter 21: Wing spars and box beams Chapter 22: Fuselages Chapter 23: Wings Chapter 24: Fuselage frames and wing ribs Chapter 25: Laminated composite structures Section B5: Structural and loading discontinuities Chapter 26: Closed section beams Chapter 27: Open section beams Section B6: Introduction to aeroelasticity Chapter 28: Wing problems