P.P. Camanho

ORCID: 0000-0003-0363-5207
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About
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Research Areas
  • Mechanical Behavior of Composites
  • Composite Structure Analysis and Optimization
  • Fatigue and fracture mechanics
  • Composite Material Mechanics
  • Structural Analysis of Composite Materials
  • Structural Behavior of Reinforced Concrete
  • Structural Response to Dynamic Loads
  • Structural Analysis and Optimization
  • Fiber-reinforced polymer composites
  • Textile materials and evaluations
  • Numerical methods in engineering
  • Epoxy Resin Curing Processes
  • Structural Load-Bearing Analysis
  • Mechanical stress and fatigue analysis
  • Ultrasonics and Acoustic Wave Propagation
  • High-Velocity Impact and Material Behavior
  • Material Properties and Applications
  • Optical measurement and interference techniques
  • Carbon Nanotubes in Composites
  • Structural Health Monitoring Techniques
  • Probabilistic and Robust Engineering Design
  • Innovations in Concrete and Construction Materials
  • Cellular and Composite Structures
  • Natural Fiber Reinforced Composites
  • Additive Manufacturing and 3D Printing Technologies

Institute of Mechanical Engineering and Industrial Mangement
2016-2025

Universidade do Porto
2016-2025

Instituto de Ciência e Inovação em Engenharia Mecânica e Engenharia Industrial
2016-2024

Marshall Space Flight Center
2020

Seoul National University
2020

Indian Institute of Technology Kanpur
2020

Stanford University
2020

University of Lisbon
2016

National Institute of Statistics and Geography
2005-2010

Japan External Trade Organization
2007

A new decohesion element with the capability of dealing crack propagation under mixed-mode loading is proposed and demonstrated. The used at interface between solid finite elements to model initiation non-self-similar growth delaminations in composite materials. single relative displacement-based damage parameter applied a softening law track state prevent restoration cohesive during unloading. three-parameter Benzeggagh-Kenane mode interaction criterion predict delamination propagation. To...

10.1177/0021998303034505 article EN Journal of Composite Materials 2003-08-01

A three-dimensional finite element model is developed to predict damage progression and strength of mechanically fastened joints in carbon fibre-reinforced plastics that fail the bearing, tension shear-out modes. The based on a model, failure criterion constitutive equation takes into account effects material elastic properties. This accomplished using internal state variables are functions type damage. formulation used together with global ultimate joint. Experimental results concerning...

10.1177/002199839903302402 article EN Journal of Composite Materials 1999-12-01

A new set of six phenomenological failure criteria for fiber-reinforced polymer laminates denoted LaRC03 is described. These can predict matrix and fiber accurately, without the curve-fitting parameters. For under transverse compression, angle fracture plane solved by maximizing Mohr-Coulomb effective stresses. criterion kinking obtained calculating misalignment load applying in coordinate frame misalignment. Fracture mechanics models cracks are used to develop a tension calculate associated...

10.1177/0021998305046452 article EN Journal of Composite Materials 2005-01-25

10.1016/j.compositesa.2006.11.009 article EN Composites Part A Applied Science and Manufacturing 2007-01-18

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

10.1016/j.compscitech.2006.02.017 article EN Composites Science and Technology 2006-04-05
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