Results 101 to 110 of about 18,796 (217)
Design exploration methodology for ultra thick laminated composites [PDF]
, 2012 Existing test and analytical methods (theoretical and numerical) are normally restricted to thin laminate components, which cannot accurately represent the 3D stress state behaviour of the so called Ultra Thick Laminates (UTL) structures.
Carrasco-Munoz Y Guerra, Jacinto
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Vibration Excitation and Suppression of a Composite Laminate Plate Using Piezoelectric Actuators. [PDF]
Materials (Basel), 2022 Her SC, Chen HY.
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Hybrid composite laminate structures
, 1977 An invention which relates to laminate structures and specifically to essentially anisotropic fiber composite laminates is described. Metal foils are selectively disposed within the laminate to produce increased resistance to high velocity impact ...
Lark, R. F., Chamis, C. C.
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Thermoelastic stress analysis of laminated composite materials
, 2009 In this work thermoelastic stress analysis (TSA) is used to obtain quantitative stress/strain data from a variety of multi-directional laminated composites. In order to interpret the thermoelastic signal correctly the source of the thermoelastic response
Sambasivam, Shamala
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Failure map of composite laminate mechanical joint
, 2007 The aim of this research is to investigate the pin/hole contact stress of a composite laminate and failure modes when submitted to tensile bearing tests.
DI BELLA, Guido +4 more
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Pre-stressed advanced fibre reinforced composites fabrication and mechanical performance [PDF]
, 2006 Advanced composite materials have high strength-to-weight ratios, corrosion resistance and durability and are extensively used in aerospace, energy and defence industries. This research concentrates on minimising the process-induced residual stresses,
Krishnamurthy, S.
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Virtual assessment of a composite laminate with interleaved nanofibrous mat under impact loading
, 2014 This paper deals with interleaving a nanofibrous mat between laminate plies to control the interlaminar delamination strength. In previous works, the authors tested delamination toughness and identified the cohesive zone properties of nanomats with ...
Giuliese, G. +11 more
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Flutter behaviour of composite aircraft wings [PDF]
, 1999 This research work presents series of investigations into the structural dynamics and dynamic aeroelastic (flutter) behaviour of composite and metal wings.
Ashawesh, Gamal Mohamed
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, 2017 © 2017 Elsevier Ltd Aircraft skin panels stiffened with attached stiffeners are commonly used in aerospace design. Recent interest on investigations of supersonic flutter of composite panels have concentrated on developments to deal with typical ...
Marques, FD, Ferreira, AJM, Natarajan, S
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Ultrasonic Guided Wave Testing on Cross-Ply Composite Laminate: An Empirical Study. [PDF]
Sensors (Basel), 2020 Aranguren G +4 more
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