Aeroelastic Vibrations and Stability of Plates and Shells

Igor A. Kijko

ISBN 10: 311033836X / ISBN 13: 9783110338362

Published by De Gruyter, De Gruyter Nov 2014, 2014

About this Item

This item is printed on demand - Print on Demand Titel. Neuware -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).De Gruyter Mouton, Genthiner Straße 13, 10785 Berlin 234 pp. Englisch.

Seller Inventory # 9783110338362

Bibliographic Details

• Title: Aeroelastic Vibrations and Stability of Plates and Shells
• Publisher: De Gruyter, De Gruyter Nov 2014
• Publication Date: 2014
• Language: English
• ISBN 10: 311033836X
• ISBN 13: 9783110338362
• Binding: Buch
• Condition: Neu
• Dimensions: 246W x 175H x 19D millimeters 246 millimeters width by 175 millimeters height by 19 millimeters depth
• Weight: 583 grams

About this title

Synopsis

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).

About the Author

Sergey D. Algazin, Ishlinsky Institute of Problems of Mechanics, Russia.
Igor A. Kijko, Moscow State University, Russia.