The paper summarizes the recent activities performed at inside FP7-NOVEMOR project related to the application of morphing technologies and in particular the variable camber concept. After a short reminder on the tools developed aiming at the design of variable camber morphing wings, the paper describes the main results obtained from the application of this morphing concept to a typical regional aircraft. Finally, the validation activities by means of the wind tunnel test campaigns are briefly introduced.

Application of the Morphing Camber Concept to a Regional Aircraft

DE GASPARI, ALESSANDRO;RICCI, SERGIO;
2014-01-01

Abstract

The paper summarizes the recent activities performed at inside FP7-NOVEMOR project related to the application of morphing technologies and in particular the variable camber concept. After a short reminder on the tools developed aiming at the design of variable camber morphing wings, the paper describes the main results obtained from the application of this morphing concept to a typical regional aircraft. Finally, the validation activities by means of the wind tunnel test campaigns are briefly introduced.
2014
4th EASN Association International Workshop on Flight Physics and Aircraft Design
morphing structures; compliant mechanism; aero-structural optimization, wind tunnel testing.
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11311/987213
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