| KEYWORD |
Wing Optimization Driven by Aeroelasticity
Thesis abroad
keywords AEROELASTICITY
Reference persons ENRICO CESTINO, GIACOMO FRULLA
External reference persons Emmanuel Benard, ISAE-SUPAERO
Joseph Morlier, ISAE SUPAERO-CNRS-INSA-Mines Albi-UPS
Research Groups 21-Progetto di velivoli e strutture aerospaziali in materiale composito
Thesis type THEORETICAL AND SIMULATION
Description The selected candidate will be asked to interface with the just described design framework to perform optimizations driven by aeroelastic parameters. The evolution of a conventional wing design will be analyzed for two main conditions: assuming the enhancement of the flutter speed as the objective function and minimizing the structural weight by fixing the flutter speed as the optimization constraint.
See also proposal for internship_isae.pdf
Required skills Python user
Preliminary design
FEM
Aeroelasticity
Notes Funding and free accommodation may be provided by ISAE-SUPAERO
Deadline 12/09/2018
PROPONI LA TUA CANDIDATURA