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Wing Optimization Driven by Aeroelasticity

estero 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