Aircraft structures for engineering students / T.H.G. Megson.
Material type:
TextSeries: Elsevier aerospace engineering series: Publisher: Amsterdam ; Boston : Butterworth-Heinemann is an imprint of Elsevier, [2017]Edition: Sixth editionDescription: xvii, 891 pages : illustrations ; 24 cmContent type: text Media type: unmediated Carrier type: volumeISBN: 9780081009147; 0081009143Subject(s): Airframes -- Textbooks | Structural analysis (Engineering) -- Textbooks | Airframes | Structural analysis (Engineering) | Avions -- Conception et construction | Avions -- VibrationsGenre/Form: Textbooks.DDC classification: 629.13431 LOC classification: TL671.6 | .M36 2017| Item type | Current location | Home library | Shelving location | Call number | Status | Date due | Barcode | Item holds |
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Book
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School of Mechanical & Manufacturing Engineering (SMME) | School of Mechanical & Manufacturing Engineering (SMME) | Aerospace Engineering | 629.13431 MEG (Browse shelf) | Available | SMME-4346 |
Includes index.
Part A. Fundamentals of structural analysis. Section A1. Elasticity. Basic elasticity -- Two-dimensional problems in elasticity -- Torsion of solid sections -- Section A2. Virtual work, energy, and matrix methods. Virtual work and energy methods -- Energy methods -- Matrix methods -- Section A3. Thin plate theory. Bending of thin plates -- Section A4. Structural instability. Columns -- Thin plates -- Section A5. Vibration of structures. Structural vibration -- -- Part B. Analysis of aircraft structures. Section B1. Principles of stressed skin construction. Materials -- Structural components of aircraft -- Section B2. Airworthiness and airframe loads. Airworthiness -- Airframe loads -- Fatigue -- Section B3. Bending, shear and torsion of thin-walled beams. Bending of open and closed, thin-walled beams -- Shear of beams -- Torsion of beams -- Combined open and closed section beams -- Structural idealization -- Section B4. Stress analysis of aircraft components. Wing spars and box beams -- Fuselages -- Wings -- Fuselage frames and wing ribs -- Laminated composite structures -- Section B5. Structural and loading discontinuities. Closed section beams -- Open section beams -- Section B6. Introduction to aeroelasticity. Wing problems -- Appendix : Design of a rear fuselage.
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