Skip to main content
Book Chapter

Distributed Actuation and Control of a Morphing Wing Trailing Edge

  • Dimino I
  • Ciminello M
  • Concilio A
  • et al.
Springer International Publishing, (2016), 171-186
DOI: 10.1007/978-3-319-22413-8_9
N/ACitations
Citations of this article
7Readers
Mendeley users who have this article in their library.
Get full text

Abstract

In a morphing wing trailing edge device, the actuated system stiffness, load capacity, and integral volumetric requirements drive flutter, actuation strength, and aerodynamic performance. Design...

Cite

CITATION STYLE

APA

Dimino, I., Ciminello, M., Concilio, A., Pecora, R., Amoroso, F., Magnifico, M., … Zivan, L. (2016). Distributed Actuation and Control of a Morphing Wing Trailing Edge. In Smart Intelligent Aircraft Structures (SARISTU) (pp. 171–186). Springer International Publishing. https://doi.org/10.1007/978-3-319-22413-8_9

Register to see more suggestions

Mendeley helps you to discover research relevant for your work.

Already have an account?

Save time finding and organizing research with Mendeley

Sign up for free