Smart morphing and sensing for aeronautical configurations : prototypes, experimental and numerical findings from the H2020 N° 723402 SMS EU project

Smart morphing and sensing for aeronautical configurations : prototypes, experimental and numerical findings from the H2020 N° 723402 SMS EU project / Marianna Braza, Jean-François Rouchon, George Tzabiras, Franco Auteri, Pawel Flaszynski, editors.

This book reports on advanced strategies to design, modeling and testing morphing wings for aeronautical applications. Covering the major outcomes of the multidisciplinary project "Smart Morphing & Sensing" (BH2020 N 723402 SMS), funded by the European Union between 2017 and 2020, it p...

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Bibliographic Details
Other Authors: Braza, Marianna (Editor), Rouchon, Jean-François (Editor), Tzabiras, G. (George) (Editor), Auteri, Franco (Editor), Flaszynski, Pawel (Editor)
Format: eBook
Language:English
Published: Cham : Springer, 2023.
Series:Notes on numerical fluid mechanics and multidisciplinary design ; v. 153.
Subjects:
Airplanes > Wings > Design and construction.
Airplanes > Wings > Testing.
Airplanes > Wings > Mathematical models.
Computational fluid dynamics.
Airplanes > Wings > Design and construction
Airplanes > Wings > Mathematical models
Airplanes > Wings > Testing
Computational fluid dynamics
Online Access:Click for online access
Table of Contents:
  • Prototypes and electroactive actuators design
  • Subsonic regime sRS wing
  • Transonic regime tRS wing
  • Sensing
  • Control law definition
  • Experimental study of the aerodynamic performance increase Subsonic regime
  • Transonic regime
  • Prototype and actuator design
  • Sensing multipoint system through Bragg grating
  • Control law definition
  • Experimental study - characterization of the LS in take-off conditions
  • Advanced CFD
  • Structural mechanics involving electroactive properties
  • Numerical results on the sRS prototype: take-off conditions
  • Numerical results on the tRS prototype: cruise conditions
  • Numerical results on the LS prototype: take-off and landing
  • Sensitivity analysis through adjoined-based MDO
  • Numerical results on the whole aircraft (morphing A320)
  • Synthesis on the numerical simulations major outcomes
  • sRS control for aerodynamic performance increase
  • tRS final experimental evaluation in cruise
  • LS final experimental evaluation in take-off and landing
  • Synthesis on the final demonstrators.

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