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Mechanics of Aircraft Structures, by C. T. Sun
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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.
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
- 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.
- Sales Rank: #1499769 in Books
- Published on: 1998-03-30
- Original language: English
- Number of items: 1
- Dimensions: 9.47" h x .76" w x 6.18" l, .0 pounds
- Binding: Hardcover
- 272 pages
From the Publisher
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.
From the Back Cover
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.
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
- 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.
About the Author
C. T. SUN is the Neil Armstrong Distinguished Professor at Purdue University. His experience spans three decades, and he has received a number of teaching and research awards in aeronautics and composite materials.
Most helpful customer reviews
27 of 29 people found the following review helpful.
Is it possible to give 0 stars?
By Jeff Maurer
Wow..... It's shocking that a book this poor could actually reach publication.
This book appears to consist of a collection of the author's teaching notes. Highly mathematical (fine), but utterly lacking in the "what this formula means in the real world" department. Aren't we as students trying to understand where all the math is leading us?
Most annoying of all, throughout the book the author uses the following: "It is easy to prove that..." Well, I'm sure it is easy for him to prove it. He's the f'ing teacher. But for us, the students, it's NOT trivial, nor should it be treated as such.
I concur with the other review. Stay as far away from this text as possible.
17 of 17 people found the following review helpful.
TOTAL WASTE OF MONEY
By F. Ch�nard
I HAD TO BUY THIS BOOK FOR MY STRUCTURE CLASS IN AEROSPACE ENGINEERING; PAYING SO MUCH FOR SO LITTLE REALLY AGGRAVATED ME. THIS BOOK HAS NO CONTENT, THERE IS NO APPLICATION TO REAL LIFE PROBLEMS, IT IS PURE GARBAGE. THE TEACHER FOLLOWED EXACTLY THIS TEXTBOOK FOR HIS CLASS; I DON'T KNOW MORE ABOUT AIRCRAFT STRUCTURES THAN I DID BEFORE TAKING THAT CLASS. 1 STAR IS WAY TOO MUCH!!! STAY AWAY FROM IT!!!!!!!!
9 of 9 people found the following review helpful.
The Good and the Bad, mostly the Bad.
By Stephen Beirne
I was required to purchase this book for my Junior level A&AE Structural Analysis Course. Chock full of theory and derivations, it doesn't set forth a clear path for learning, but rather a thicket in which problems sets are solved by wildly searching backward in the book for equations and examples in order to help make some sense of the problem at hand. While the book is full of good problems, the concepts tested in the problems are not always clearly explained (What the heck is shear flow anyway?).
This book is recommended as a junior or senior level structures text, but how well it is received depends highly upon the Professor's lecture style (Straight from the text?(=bad) or supplemental to the text?(=not as bad)).
The Bad outweigh the Good.
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