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Aircraft Structures for Engineering Students - T.H.G. Megson

Aircraft Structures for Engineering Students

(Autor)

Buch | Softcover
824 Seiten
2007 | 4th edition
Butterworth-Heinemann Ltd (Verlag)
978-0-7506-6739-5 (ISBN)
CHF 106,45 inkl. MwSt
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Covers various fundamental subjects, including elasticity, structural analysis, airworthiness and aeroelasticity. This book includes a Solutions Manual available to various adopting teachers, and organization aids understanding of the fundamentals of structural analysis and emphasizes applications to aircraft structures.
Aircraft Structures for Engineering Students is the leading self contained aircraft structures course text. It covers all fundamental subjects, including elasticity, structural analysis, airworthiness and aeroelasticity. Now in its fourth edition, the author has revised and updated the text throughout and added new case study and worked example material to make the text even more accessible.

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.

Part A. Basic Elasticity. Two-Dimensional Problems in Elasticity. Torsion of Solid Sections. Virtual Work. Energy Methods. Strain Energy and Complementary Energy. Matrix Methods. Bending of Thin Plates. Columns. Thin Plates. Tension Field Beams. Flexural-Torsional Buckling of Thin Walled Columns. Structural Vibration. Part B. Materials. Structural Components of Aircraft. Airworthiness. Airframe Loads. Fatigue. Bending of Beams. Shear of Beams. Torsion of Beams. Analysis of Combined Open and Closed Section Beams. Structural Idealisation. Wing Spars and Box Beams. Fuselages. Wings. Fuselage Frames and Wing Ribs. Laminated Composite Structures. Closed Section Beams. Open Section Beams. Wing Problems. APPENDIX Case Study: Design of an Aircraft Fuselage.

Erscheint lt. Verlag 2.3.2007
Verlagsort Oxford
Sprache englisch
Maße 189 x 246 mm
Gewicht 1560 g
Themenwelt Technik Fahrzeugbau / Schiffbau
Technik Luft- / Raumfahrttechnik
ISBN-10 0-7506-6739-7 / 0750667397
ISBN-13 978-0-7506-6739-5 / 9780750667395
Zustand Neuware
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