Development and execution of new test procedures for thermoplastic aircraft fuselage panels

The main objective of the topic is to validate the structural behavior of thermoplastic aircraft fuselage panels in relation to new analytical methods for out of autoclave thermoplastic curing processes by static testing of panels under representative loads conditions. The tests will ensure the improved understanding of the structural response of the developed concept and proper design solutions for future application. Please refer to the full topic descriptions document published in this call.