This paper presents preliminary results about the design and optimization of a model-scale active twist blade actuated by means of Macro Fiber Composites (MFC), as part of the EU-sponsored Friendcopter project for an environmentally friendly helicopter. The capability to numerically characterize induced strain composite beam sections is used in an optimization problem to determine the design of the rotor blade, which will be subsequently experimented in a hover test rig at DLR.

Optimal Design of an Active Twist 1:2.5 Scale Rotor Blade

MASARATI, PIERANGELO;MORANDINI, MARCO;
2005-01-01

Abstract

This paper presents preliminary results about the design and optimization of a model-scale active twist blade actuated by means of Macro Fiber Composites (MFC), as part of the EU-sponsored Friendcopter project for an environmentally friendly helicopter. The capability to numerically characterize induced strain composite beam sections is used in an optimization problem to determine the design of the rotor blade, which will be subsequently experimented in a hover test rig at DLR.
2005
31st European Rotorcraft Forum
File in questo prodotto:
Non ci sono file associati a questo prodotto.

I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.

Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11311/252108
Citazioni
  • ???jsp.display-item.citation.pmc??? ND
  • Scopus 17
  • ???jsp.display-item.citation.isi??? ND
social impact