LM

L Morino

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5 records found

Sequential Multi-Disciplinary Optimization for the Conceptual Design of a Blended-Wing-Body Aircraft
The objective of the present work is the preliminary sizing of a BWB (Blended Wing Body) passenger aircraft configuration, using a multidisciplinary modelling and optimization methodology. The aim is to ensure that all the important aspects of the design are taken into account in ...

A viscous-flow decomposition with aerodynamic and aeroelastic applications

A Computational Formulation for the Analysis of Viscous Flows with Aeroelastic Applications
Conference paper - G Arsuffi, M. Baragona, G Bernardini, L Morino

Conceptual design of a blended wing body aircraft

A Hermite high-order finite element for structural optimal design
Conference paper - L Morino, G Bernardini, C Cerulli, F Cetta