Smart Morphing and Sensing for Aeronautical Configurations Prototypes, Experimental and Numerical Findings from the H2020 N° 723402 SMS EU Project /

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” (H2020 N° 723402 SMS), funded by the European Union between 2017 and 2020, it presents a...

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Kaydedildi:
Detaylı Bibliyografya
Müşterek Yazar: SpringerLink (Online service)
Diğer Yazarlar: Braza, Marianna (Editör), Rouchon, Jean-François (Editör), Tzabiras, George (Editör), Auteri, Franco (Editör), Flaszynski, Pawel (Editör)
Materyal Türü: Elektronik Ekitap
Dil:İngilizce
Baskı/Yayın Bilgisi: Cham : Springer International Publishing : Imprint: Springer, 2023.
Edisyon:1st ed. 2023.
Seri Bilgileri:Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 153
Konular:
Online Erişim:https://doi.org/10.1007/978-3-031-22580-2
Etiketler: Etiketle
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İçindekiler:
  • 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
  • Synthesison the final demonstrators.