@inproceedings{a24b4350c1a849b3937de819c46c3e84,
title = "Static test of a thermoplastic compositewingbox under shear and bending moment",
abstract = "The proof of an aircraft{\textquoteright}s structural integrity and safety is typically provided by analysis and supported by structural test evidence. The experimental test of a wingbox, which is the main structural component of a wing, can provide useful data on assessment of its structural performance in an actual airplane for the design objectives. To this end, a testing fixture was designed and manufactured to introduce a prescribed shear force and bending moment at one end of a variable stiffness thermoplastic composite wingbox and react the load at the other end. We report experimental results and compare them with detailed finite element data.",
author = "Giovanni Zucco and Vincenzo Oliveri and Dani{\"e}l Peeters and Robert Telford and Gearoid Clancy and Ciaran McHale and Mohammad Rouhi and Ronan O{\textquoteright}Higgins and Young, {Trevor M.} and Weaver, {Paul M.}",
note = "Publisher Copyright: {\textcopyright} 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018 ; Conference date: 08-01-2018 Through 12-01-2018",
year = "2018",
doi = "10.2514/6.2018-0482",
language = "English",
isbn = "9781624105326",
series = "AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials",
}