Non-linear vibrations of variable stiffness composite laminated plates

By Pedro Manuel Santos Ribeiro, Hamed Akhavan. 2012

145 citations recorded by the source corpus.

Subfields: Civil and Structural Engineering, Control and Systems Engineering, Mechanics of Materials

View Paper: https://www.semanticscholar.org/paper/163317ac279243650236fdaba21db5dab709e2f9

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Civil and Structural Engineering

1. Paul M. Weaver
2. Paul Kealy
3. J. Cooper
4. O. Stodieck
5. Pedro Manuel Santos Ribeiro
6. Jerzy Warminski
7. Hamed Akhavan
8. A. Teter

In Control and Systems Engineering

1. Paul Kealy
2. J. Cooper
3. Paul M. Weaver
4. O. Stodieck
5. Hamed Akhavan

In Mechanics of Materials

1. Paul M. Weaver
2. Paul Kealy
3. J. Cooper
4. O. Stodieck
5. Pedro Manuel Santos Ribeiro
6. Jerzy Warminski
7. Hamed Akhavan
8. A. Teter

Citations in the corpus

• A review on the mechanical behaviour of curvilinear fibre composite laminated panels (2014, background): “In free vibrations, different internal resonances appeared due to the curvilinear fibres.(71) In forced vibrations,(72) it was found that, at least in some situations, curvilinear fibres lead to lower vibration amplitudes.”
• Improved aeroelastic tailoring using tow-steered composites (2013, methodology): “Within the bounds of the parametric study, the maximum flutter speed of the plate was achieved for a VAT layup of Root[ 45 45 45 45]s/ Tip[ 27 27 45 45]s, as well as for a non-standard UD laminate of [ 36 36 45 45]s, which was 14% higher than the maximum aeroelastic instability airspeed for a standa”