Mechanics of Aircraft Structures
Book Description
The concept of postbuckling of thin rods
Mechanics of composite materials and laminates.
Aircraft structures must be designed to ensure that every part of a given material is used to its full capacity; today's designs employ cutting-edge composite materials to meet those needs. This book focuses on the mechanics of the most recent developments in design and materials, and covers advanced composite materials and new computer-aided designs.
Book Details
Hardcover: 255 pages
Publisher: Wiley-Interscience (March 16, 1998)
Language: English
ISBN-10: 0471178772
ISBN-13: 978-0471178774
An accessible, state-of-the-art introduction to the most important topics in aerospace engineering today
This combined text and professional reference presents what every structural engineer needs to know about modern aircraft structures. Covering the latest developments in the field, it explores the role of commercial finite element codes in structural analysis, demonstrates the use of fracture mechanics to solve damage tolerance and durability problems in aircraft structures, and examines the penetration of composite materials into areas traditionally dominated by metals. Clear and accessible throughout, this book assumes only an introductory background in the mechanics of solids while explaining subjects typically found only in much more advanced texts. It offers ample examples, emphasizes concepts of mechanics rather than problem solving,and helps foster an in-depth understanding of the subject.
This combined text and professional reference presents what every structural engineer needs to know about modern aircraft structures. Covering the latest developments in the field, it explores the role of commercial finite element codes in structural analysis, demonstrates the use of fracture mechanics to solve damage tolerance and durability problems in aircraft structures, and examines the penetration of composite materials into areas traditionally dominated by metals. Clear and accessible throughout, this book assumes only an introductory background in the mechanics of solids while explaining subjects typically found only in much more advanced texts. It offers ample examples, emphasizes concepts of mechanics rather than problem solving,and helps foster an in-depth understanding of the subject.
Mechanics of Aircraft Structures provides concise introductions to:
Aerospace materials —advanced composites as well as metals
The concept of anisotropy in material properties and properties of fiber composites
A new approach for deriving the shear flow on thin-walled sections
Methods for calculating strain energy release rates and stress intensity factors for simple structures
Fracture mechanics topics —fatigue crack growth and fiber-reinforced composites Aerospace materials —advanced composites as well as metals
The concept of anisotropy in material properties and properties of fiber composites
A new approach for deriving the shear flow on thin-walled sections
Methods for calculating strain energy release rates and stress intensity factors for simple structures
The concept of postbuckling of thin rods
Mechanics of composite materials and laminates.
Mechanics of Aircraft Structures combines classical and state-of-the-art topics into an excellent one-semester introductory course in structural mechanics and aerospace engineering at the undergraduate or graduate level. It is also an extremely useful resource for aerospace or mechanical engineers —especially in aerospace, automotive, and defense-related industries.
From the PublisherAircraft structures must be designed to ensure that every part of a given material is used to its full capacity; today's designs employ cutting-edge composite materials to meet those needs. This book focuses on the mechanics of the most recent developments in design and materials, and covers advanced composite materials and new computer-aided designs.
Book Details
Hardcover: 255 pages
Publisher: Wiley-Interscience (March 16, 1998)
Language: English
ISBN-10: 0471178772
ISBN-13: 978-0471178774
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