Prof. Alberto Guardone
Current affiliation: Politecnico di Milano
Subject: Aeronautics
Primary location: Italy
Multifidelity Physics-Based Method for Robust Optimization Applied to a Hovering Rotor Airfoil
Published in:AIAA Journal
Publication date:2015-11-01
Robust aerodynamic optimization of morphing airfoils for helicopter rotor blades
Published in:17th AIAA Non-Deterministic Approaches Conference
Publication date:2015-01-02
Drag minimization of an isolated airfoil in transonic inviscid flow by means of genetic algorithms
Published in:53rd AIAA Aerospace Sciences Meeting
Publication date:2015-01-03
Evidence of complex flow structures in a converging-diverging nozzle caused by a recessed step at the nozzle throat
Published in:45th AIAA Fluid Dynamics Conference
Publication date:2015-06-18
Extension of the SU2 open source CFD code to the simulation of turbulent flows of fuids modelled with complex thermophysical laws
Published in:22nd AIAA Computational Fluid Dynamics Conference
Publication date:2015-06-18
A model for in-flight ice accretion based on the exact solution of the unsteady Stefan problem
Published in:7th AIAA Atmospheric and Space Environments Conference
Publication date:2015-06-18
An Adaptive Conservative ALE Approach to Deal with Large Boundary Displacements in Three-Dimensional Inviscid Simulations
Published in:55th AIAA Aerospace Sciences Meeting
Publication date:2017-01-05
Blockage and Three-Dimensional Effects in Wind-Tunnel Testing of Ice Accretion over Wings
Published in:Journal of Aircraft
Publication date:2017-03-01
Local Solution to the Unsteady Stefan Problem for In-Flight Ice Accretion Modeling
Published in:Journal of Aircraft
Publication date:2018-01-01
Influence of a recessed step at the throat section of a supersonic nozzle
Published in:The Aeronautical Journal
Publication date:2018-02-20