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Faserstoff
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Bio-based hybrid cabin door of ultralight helicopter with variable-axis fiber design
Sensor based online quality monitoring system for detection of milling defects on CFRP structures
Sensor based online quality monitoring system for detection of milling defects on CFRP structures
Outlook on ecologically improved composites for aviation interior and secondary structures
Outlook on ecologically improved composites for aviation interior and secondary structures
G-1(Invited) Si Microphotonics
Morphing wing flexible skins with curvilinear fiber composites
Experimental investigation and design of a shape-variable compressor cascade
Experimental investigation and design of a shape-variable compressor cascade
BEARING, PLAIN, ROD END, SELF-ALIGNING, SELF-LUBRICATING,WIDE, EXTERNALLY THREADED, -65 TO +325 °F
BEARING, PLAIN, ROD END, SELF-ALIGNING, SELF-LUBRICATING, WIDE, INTERNALLY THREADED, −65 TO +325 °F
Structural optimisation of random discontinuous fibre composites: Part 2 – Case study
In-situ structural evaluation during the fibre deposition process of composite manufacturing
In-situ structural evaluation during the fibre deposition process of composite manufacturing
Pattern design and optimization for filament-wound toroidal pressure vessels
Investigation into the effects of fiber waviness in standard notched composite specimens
Investigation into the effects of fiber waviness in standard notched composite specimens
Driven dynamics of time-varying linear systems
Reliability monitoring of broadband access networks
Design of FML shear panels for ultra-high capacity aircraft
Probabilistic theories of time dependent failure of fiber bundles
Estimation of sealability with compressed fibers sheet gaskets for liquid and gas fluid
FEA and testing studies on static camber performance of the radial tire
Aeroelastic tailoring of an NLF forward swept wing
Aeroelastic tailoring of an NLF forward swept wing
Structural analysis and testing of composites in automotive crashworthiness application
Activities of the University of Toronto Institute for Aerospace Studies
Review of Classical Laminated Plate Theory
Cost of Composites: A Qualitative Discussion