Aeroelastic Vibrations and Stability of Plates and Shells
Seiten
2014
De Gruyter (Verlag)
978-3-11-033836-2 (ISBN)
De Gruyter (Verlag)
978-3-11-033836-2 (ISBN)
The DeGruyter Studies in Mathematical Physics are devoted to the publication of monographs and high-level texts in mathematical physics. They cover topics and methods in fields of current interest, with an emphasis on didactical presentation. The series will enable readers to understand, apply and develop further, with sufficient rigor, mathematical methods to given problems in physics. For this reason, works with a few authors are preferred over edited volumes. The works in this series are aimed at advanced students and researchers in mathematical and theoretical physics. They also can serve as secondary reading for lectures and seminars at advanced levels.
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).
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).
Sergey D. Algazin, Ishlinsky Institute of Problems of Mechanics, Russia.Igor A. Kijko, Moscow State University, Russia.
| Erscheint lt. Verlag | 17.11.2014 |
|---|---|
| Reihe/Serie | De Gruyter Studies in Mathematical Physics ; 25 |
| Zusatzinfo | 35 b/w ill., 25 b/w tbl. |
| Verlagsort | Berlin/Boston |
| Sprache | englisch |
| Maße | 170 x 240 mm |
| Gewicht | 532 g |
| Themenwelt | Naturwissenschaften ► Physik / Astronomie ► Strömungsmechanik |
| Naturwissenschaften ► Physik / Astronomie ► Theoretische Physik | |
| Schlagworte | aerodynamics • Aeroelastizität • Automation • Automotive • Cicero • Damping • Dünnwandiges Bauelement • Dynamics • Elastic plates and shells • Mathematical & Computational • Mathematical Physics • Mechanics • Mechanics and Fluid Dynamics • Mechatronics and Automotive • Physics • Plates (Engineering) • Platte • Schale • Science • Shells (Engineering) • stability • TECHNOLOGY & ENGINEERING • Theoretical and Mathematical Physics • theoretical physics • Theoretische Physik • TUSC • ÜBERALTER • Vibration |
| ISBN-10 | 3-11-033836-X / 311033836X |
| ISBN-13 | 978-3-11-033836-2 / 9783110338362 |
| Zustand | Neuware |
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