P. Robinson

ORCID: 0000-0003-3649-587X
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About
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Research Areas
  • Mechanical Behavior of Composites
  • Structural Behavior of Reinforced Concrete
  • Fiber-reinforced polymer composites
  • Structural Response to Dynamic Loads
  • Fatigue and fracture mechanics
  • Structural Analysis of Composite Materials
  • Cellular and Composite Structures
  • Composite Structure Analysis and Optimization
  • Structural Analysis and Optimization
  • Laser and Thermal Forming Techniques
  • Ultrasonics and Acoustic Wave Propagation
  • High-Velocity Impact and Material Behavior
  • Mechanical stress and fatigue analysis
  • Composite Material Mechanics
  • Textile materials and evaluations
  • Aeroelasticity and Vibration Control
  • Numerical methods in engineering
  • Epoxy Resin Curing Processes
  • Structural Load-Bearing Analysis
  • Smart Materials for Construction
  • Structural Health Monitoring Techniques
  • Isotope Analysis in Ecology
  • Natural Fiber Reinforced Composites
  • Additive Manufacturing and 3D Printing Technologies
  • Polymer composites and self-healing

Imperial College London
2012-2024

REVA University
2021

AstraZeneca (United Kingdom)
2006-2018

University of Florida
2013

Google (United States)
2012

Loughborough University
2011

Wheaton College - Massachusetts
2006

Louisiana State University
1992-2001

McDermott International (United States)
2000-2001

Louisiana State University Agricultural Center
1991

This paper presents a pressure-dependent three-dimensional constitutive law to predict failure for laminated composites. The nonlinear response in shear and the transverse through-the-thickness directions, which is measured experimentally, incorporated directly into model. In addition, secant stiffnesses are dependent on state of hydrostatic pressure general strain. criteria distinguish between matrix failure, fibre kinking tensile failure. In-situ strengths used Propagation takes...

10.1177/0021998312454478 article EN Journal of Composite Materials 2012-09-01

This article showcases the authors’ predictions for Part B of second World Wide Failure Exercise. Predictions are made using failure criteria published in submission A. In several cases, original found to match experimental data well and no revisions made. A novel constitutive model unidirectional composite materials is used improve cases involving multidirectional laminates.

10.1177/0021998313476523 article EN Journal of Composite Materials 2013-02-20

The inherent brittleness of continuous unidirectional fibre reinforced composites is a major drawback to their otherwise outstanding mechanical performance. This paper exploits with overlapped discontinuities at the ply level create significantly non-linear response, due progressive interlaminar damage under tensile loading. Two distinct configurations were manufactured same carbon/epoxy system and tested quasi-static tension, showing that varying thickness length overlapping blocks resulted...

10.1016/j.compscitech.2014.10.022 article EN cc-by Composites Science and Technology 2014-11-01

A detailed study of the Mode I interlaminar fracture toughness measure ment multidirectional laminates is presented. The use a novel DCB specimen pro posed in which conventional delaminated along its edges by corporation inserts addition to usual delamination at loaded end. Investigations using this examine +45°/+45° and +45°/-45° interfaces indicate that appropriate width edge can sup press crack jumping fibre bridging occur speci men. Preliminary tests show G IC for are significantly...

10.1177/002199839202601101 article EN Journal of Composite Materials 1992-11-01

10.1016/0734-743x(92)90408-l article EN International Journal of Impact Engineering 1992-01-01

This paper presents a computational technique for the prediction of fatigue-driven delamination growth in composite materials. The interface element, which has been extensively applied to predict due static loading, modified incorporate effects cyclic loading. Using damage mechanics formulation, constitutive law element extended by incorporating version continuum fatigue model. details degradation strategy and examples predicted mode I, II mixed I/II are presented demonstrate that numerical...

10.1002/nme.1338 article EN International Journal for Numerical Methods in Engineering 2005-01-01

10.1016/j.compositesa.2005.06.007 article EN Composites Part A Applied Science and Manufacturing 2005-09-13
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