• Publications
  • Influence
Wing-to-fuselage attachment fitting for composite airframes : experimental and finite element analysis
The design of a wing-to-fuselage attachment fitting for composite airframes is a considerable problem since it involves the application of point load to a laminate displaying a relatively low bearingExpand
  • 1
  • 1
  • PDF
Round-robin interlaminar fracture testing of carbon-fibre-reinforced epoxy and PEEK composites
Abstract This paper summarizes results from a series of tests performed in eighteen laboratories with three specific aims: first, to establish the reproducibility of values from mode I and mode IIExpand
  • 82
  • 1
NUMERICAL AND EXPERIMENTAL INVESTIGATIONS OF EMBEDDED DELAMINATION GROWTH CAUSED BY COMPRESSIVE LOADING
The paper deals with growth analysis of initially circular delaminations embedded in carbon-epoxy laminate plates subjected to compressive loading. Three different reinforcement lay-ups yieldingExpand
  • 7
  • 1
Trigeminal Medullary Dorsal Horn Neurons Activated by Nasal Stimulation Coexpress AMPA, NMDA, and NK1 Receptors
Afferent information initiating the cardiorespiratory responses during nasal stimulation projects from the nasal passages to neurons within the trigeminal medullary dorsal horn (MDH) via the anteriorExpand
  • 3
  • PDF
Properties of Adhesives and their Applications
Abstract The stress analysis of an adhesively bonded lap joint requires more information on the mechanical properties of adhesives than it is normally furnished by the manufacturers. For this reasonExpand
  • 4
Material studies of composites by automatic grating interferometry
High-sensitivity grating interferometry is shown as the effective experimental tool for the composite material characterization, biaxial testing, stress and failure analysis. The hardware andExpand
  • 4
Effect of reinforcement arrangement on distribution of GI, GII and GIII along fronts of circular delaminations in orthotropic composite plates
Abstract The relationships between the distributions of the Strain Energy Release Rate components and the reinforcement arrangements in delamination separated layers of polymeric laminate wereExpand
  • 4
NUMERICAL SIMULATION OF FATIGUE DELAMINATION GROWTH UNDER MODE I LOADING CONDITIONS
Delaminations are common defects that deteriorate strength of laminates. Delaminations can arise in the course of manufacturing due to faulty fabrication process or can result from low energyExpand
  • 4
  • PDF