๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Transient response of stiffened composite plates subjected to low velocity impact

โœ Scribed by S.W. Gong; K.Y. Lam

Book ID
108494514
Publisher
Elsevier Science
Year
1999
Tongue
English
Weight
421 KB
Volume
30
Category
Article
ISSN
1359-8368

No coin nor oath required. For personal study only.

๐Ÿ“œ SIMILAR VOLUMES

Dynamic response of fully-clamped lamina
Dynamic response of fully-clamped laminated composite plates subjected to low-velocity impact of a mass
โœ Lu Chun; K.Y. Lam ๐Ÿ“‚ Article ๐Ÿ“… 1998 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 748 KB

Al~traet--A numerical method for the calculation of dynamic response of laminated composite plates under low-velocity impact is proposed. The non-linear, second-order differential governing equations are derived by the Lagrange's principle and the Hertzian contact law. The governing equations are de

NON-LINEAR TRANSIENT RESPONSE OF FLUTTER
NON-LINEAR TRANSIENT RESPONSE OF FLUTTERING STIFFENED COMPOSITE PLATES SUBJECT TO THERMAL LOAD
โœ I.K OH; I LEE; D.M LEE ๐Ÿ“‚ Article ๐Ÿ“… 2001 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 577 KB

Non-linear transient response of #uttering sti!ened composite plates subject to thermal loads has been analyzed. The "rst order shear deformable plate and Timoshenko beam theories are used for the "nite element modelling of a skin panel and sti!eners considering von Karman non-linear strain}displace