Aircraft Structures for Engineering Students
4th Edition
Published on 8. March 2007
825 pages
978-0-08-048831-8 (ISBN)
Description
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.
- The leading Aircraft Structures text, covering a complete course from basic structural mechanics to finite element analysis
- Enhanced pedagogy with additional case studies, worked examples and home work exercises
More details
Edition
4th Revised ed.
Language
English
Place of publication
San Diego
United Kingdom
Product notice
Windows
ISBN-13
978-0-08-048831-8 (9780080488318)
Copyright in bibliographic data and cover images is held by Nielsen Book Services Limited or by the publishers or by their respective licensors: all rights reserved.
Schweitzer Classification
Other editions
New editions
T. H. G. Megson
Aircraft Structures for Engineering Students
E-Book
02/2012
5th Edition
Butterworth-Heinemann
€57.95
Available for download
Additional editions
T.H.G. Megson
Aircraft Structures for Engineering Students
Book
03/2007
4th Edition
Butterworth-Heinemann
€75.51
Article exhausted; check for reprint
Persons
T.H.G. Megson was a professor emeritus with the Department of Civil Engineering at Leeds University (UK). For Elsevier he wrote 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.
Content
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.
