Aircraft Structures for Engineering Students
Edition: 4th 2007
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, 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
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All the information you need in one place! Each Study Brief is a summary of one specific subject; facts, figures, and explanations to help you learn faster.
List price: $97.95
Copyright year: 2007
Publisher: Elsevier Science & Technology Books
Publication date: 3/8/2007
Size: 7.00" wide x 9.50" long x 1.75" tall
T.H.G. Megson is a professor emeritus with the Department of Civil Engineering at Leeds University (UK).
|Fundamentals of Structural Analysis|
|Two-dimensional problems in elasticity|
|Torsion of solid sections|
|Virtual Work, Energy and Matrix Methods|
|Thin Plate Theory|
|Bending of thin plates|
|Analysis of Aircraft Structures|
|Principles of Stressed Skin Construction|
|Structural components of aircraft|
|Airworthiness and Airframe Loads|
|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|
|Fuselage frames and wing ribs|
|Laminated composite structures BV Structural and Loading Discontinuities|
|Closed section beams|
|Open section beams|
|Case Study: Design of an Aircraft Fuselage|