Aircraft Structures for Engineering Students

ISBN-10: 0750667397
ISBN-13: 9780750667395
Edition: 4th 2007
Authors: T. H. G. Megson
List price: $97.95
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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,  More...

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Book details

List price: $97.95
Edition: 4th
Copyright year: 2007
Publisher: Elsevier Science & Technology Books
Publication date: 3/8/2007
Binding: Paperback
Pages: 824
Size: 7.00" wide x 9.50" long x 1.75" tall
Weight: 3.674
Language: English

"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. Includes a Solutions Manual available to all adopting teachers. * New organization aids understanding of the fundamentals of structural analysis and emphasizes applications to aircraft structures * New worked examples throughout the text aid understanding and relate concepts to real world applications * Additional coverage includes virtual work, tension field beams, post buckling behavior, material properties, composite structures and crack propagation * An extensive aircraft design project case study shows the application of the major techniques in the book * End of chapter exercises and accompanying Instructor's Manual at http: //textbooks.elsevier.com

T.H.G. Megson is a professor emeritus with the Department of Civil Engineering at Leeds University (UK).

Fundamentals of Structural Analysis
Elasticity
Basic elasticity
Two-dimensional problems in elasticity
Torsion of solid sections
Virtual Work, Energy and Matrix Methods
Virtual work
Energy methods
Matrix methods
Thin Plate Theory
Bending of thin plates
Structural Instability
Columns
Thin plates
Structural Vibration
Analysis of Aircraft Structures
Principles of Stressed Skin Construction
Materials
Structural components of aircraft
Airworthiness and Airframe Loads
Airworthiness
Airframe loads
Fatigue
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 Idealisation B IV Stress Analysis of Aircraft Components
Wing spars and box beams
Fuselages
Wings
Fuselage frames and wing ribs
Laminated composite structures BV Structural and Loading Discontinuities
Closed section beams
Open section beams
Wing problems
Appendix
Case Study: Design of an Aircraft Fuselage

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