Studying aeroelastic behavior of aircraft with NeoCASS. : The Danbus configuration

Abstract: This Master Thesis assesses the performance of NeoCASS software as a tool for structural sizing for deformable aircraft at conceptual design level. NeoCASS is a collection of Matlab modules included in CEASIOM. Some testcases (simple wing model, TCR, Danbus, Agard 445.6 wing) are computed to evaluate the aeroelastic behavior and provide additional validation on the structural models NeoCASS computes Finally, Danbus, a new conceptual design aircraft, is analyzed with the software.