TY - GEN
T1 - Interface characterization of thermoplastic skin-stiffener composite manufactured using laser-assisted tape placement
AU - Bandaru, Aswani Kumar
AU - Clancy, Gearóid
AU - Peeters, Daniël
AU - O’Higgins, Ronan
AU - Weaver, Paul M.
N1 - Publisher Copyright:
© 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2018
Y1 - 2018
N2 - Laser-Assisted Tape Placement (LATP) is an advanced manufacturing process which has gained the attention of the aerospace industry. Composite laminates manufactured using this technique have to be characterized effectively to assess their suitability for use in structural applications. A representative skin and stiffener test coupon was manufactured using the LATP method from carbon fiber (CF) reinforced polyether ether ketone (PEEK) tapes. The main objective was to characterize the interaction between skin and stiffener in terms of interlaminar shear strength (ILSS) and fracture toughness (mode-I and mode-II) properties. For initial ILSS tests, non-unidirectional stacking sequences were used for skin and stiffener to ensure failure at their interface. Further, ILSS, double cantilever beam (DCB) and end-notched flexure (ENF) fracture toughness tests were carried out on unidirectional (UD) skin-stiffener laminates. All the mechanical tests were carried out as per ASTM standards. The values of ILSS and fracture toughness in mode-I and mode-II were comparable with the reported results stating the competence of the LATP manufactured CF/PEEK skin-stiffener.
AB - Laser-Assisted Tape Placement (LATP) is an advanced manufacturing process which has gained the attention of the aerospace industry. Composite laminates manufactured using this technique have to be characterized effectively to assess their suitability for use in structural applications. A representative skin and stiffener test coupon was manufactured using the LATP method from carbon fiber (CF) reinforced polyether ether ketone (PEEK) tapes. The main objective was to characterize the interaction between skin and stiffener in terms of interlaminar shear strength (ILSS) and fracture toughness (mode-I and mode-II) properties. For initial ILSS tests, non-unidirectional stacking sequences were used for skin and stiffener to ensure failure at their interface. Further, ILSS, double cantilever beam (DCB) and end-notched flexure (ENF) fracture toughness tests were carried out on unidirectional (UD) skin-stiffener laminates. All the mechanical tests were carried out as per ASTM standards. The values of ILSS and fracture toughness in mode-I and mode-II were comparable with the reported results stating the competence of the LATP manufactured CF/PEEK skin-stiffener.
UR - http://www.scopus.com/inward/record.url?scp=85141575847&partnerID=8YFLogxK
U2 - 10.2514/6.2018-0481
DO - 10.2514/6.2018-0481
M3 - Conference contribution
AN - SCOPUS:85141575847
SN - 9781624105326
T3 - AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018
BT - AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018
Y2 - 8 January 2018 through 12 January 2018
ER -