Comparison of High-Fidelity Aero-Structure Gradient Computation Techniques. Application on the CRM Wing Design. 1.Events, Aeroelasticity in Conceptual Aircraft Design, IFASD 2017By Beata Wierzbińska-PrusJune 13, 2024T. Achard, C. Blondeau and R. Ohayon DOI Number: N/A Conference number: IFASD-2017-002
