Experimental validation of a true-scale morphing flap for large civil aircraft applications-Reference-Cited by-同舟云学术

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Experimental validation of a true-scale morphing flap for large civil aircraft applications

Published:2017-04-04 Issue: Volume: Page:
ISSN:0277-786X
Container-title:SPIE Proceedings
language:
Short-container-title:

Author:

Pecora R.¹,Amoroso F.¹,Arena M.¹,Noviello M. C.¹,Rea F.¹

Affiliation:

1. Univ. degli Studi di Napoli Federico II (Italy)

Publisher

SPIE

Reference30 articles.

1. KRISTINA: Kinematic rib-based structural system for innovative adaptive trailing edge;Pecora,2016

2. Structural Design of an Adaptive Wing Trailing Edge for Enhanced Cruise Performance;Pecora;AIAA SciTech,2016

3. Distributed Electromechanical Actuation System Design for a Morphing Trailing Edge Wing;Dimino;SPIE Smart Structures/NDE,2016

4. Multi-Functional Morphing Trailing Edge Device for Control of All-Composite, All-Electric Flying Wing Aircraft;Wildschek,2008

5. Distributed actuation concepts for a morphing aileron device

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3. Morphing wing flaps for large civil aircraft: Evolution of a smart technology across the Clean Sky program;Chinese Journal of Aeronautics;2021-07

4. Aerodynamic Shape Design and Validation of an Advanced High-Lift Device for a Regional Aircraft with Morphing Droop Nose;International Journal of Aerospace Engineering;2019-03-27

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