04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
DEVELOPMENT OF A MASS EVALUATION TOOL FOR CLASSICAL AND DISRUPTIVE AIRCRAFT STRUCTURES
V. Priasso¹, A. Lannoo¹; ¹DMAS, ONERA, France
This presentation deals with a mass evaluation tool of an aircraft structure which uses semi-empirical and numerical models. It aims to be integrated into a Multi-Disciplinary Optimization (MDO) process for innovative aircraft. The optimization method is presented and some examples are detailed on both classical and disruptive aircraft structures.