Aeroelastic Vibrations and Stability of Plates and Shells
Language: English
Published by De Gruyter, DE, 2014
Series: Book 24 of 53 - De Gruyter Studies in Mathematical Physics
- Hardcover
- New

Seller: Rarewaves USA, HEBRON, KY, U.S.A.Rarewaves USA
AbeBooks seller since June 10, 2025
Condition: New
US$ 416.08
Quantity: Over 20 available
Add to basketItem description from seller
Back-action of aerodynamics onto structures such as wings cause vibrations and may resonantly couple to them, thus causing instabilities (flutter) and endangering the whole structure. By careful choices of geometry, materials and damping mechanisms, hazardous effects on wind engines, planes, turbines and cars can be avoided. Besides an introduction into the problem of flutter, new formulations of flutter problems are given as well as a treatise of supersonic flutter and of a whole range of mechanical effects. Numerical and analytical methods to study them are developed and applied to the analysis of new classes of flutter problems for plates and shallow shells of arbitrary plane form. Specific problems discussed in the book in the context of numerical simulations are supplemented by Fortran code examples (available on the website).
Seller Inventory # LU-9783110338362
- Title
- Aeroelastic Vibrations and Stability of Plates and Shells
- Author
- Sergey D. Algazin, Igor A. Kijko
- Publisher
- De Gruyter, DE
- Publication year
- 2014
- Condition
- New
- Binding
- Hardback
- Language
- English
- ISBN 10
- 311033836X
- ISBN 13
- 9783110338362
- Item weight
- 531 grams
- Series
- Book 24 of 53: De Gruyter Studies in Mathematical Physics
Back-action of aerodynamics onto structures such as wings cause vibrations and may resonantly couple to them, thus causing instabilities (flutter) and endangering the whole structure. By careful choices of geometry, materials and damping mechanisms, hazardous effects on wind engines, planes, turbines and cars can be avoided.
Besides an introduction into the problem of flutter, new formulations of flutter problems are given as well as a treatise of supersonic flutter and of a whole range of mechanical effects. Numerical and analytical methods to study them are developed and applied to the analysis of new classes of flutter problems for plates and shallow shells of arbitrary plane form. Specific problems discussed in the book in the context of numerical simulations are supplemented by Fortran code examples (available on the website).
"Synopsis" may belong to another edition of this title.
About the Author
Sergey D. Algazin, Ishlinsky Institute of Problems of Mechanics, Russia.
Igor A. Kijko, Moscow State University, Russia.
"About the title" may belong to another edition of this title.
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