LEADER 04123nam 2200505 450 001 9910672441703321 005 20230522084109.0 010 $a3-031-22580-5 024 7 $a10.1007/978-3-031-22580-2 035 $a(MiAaPQ)EBC7207053 035 $a(Au-PeEL)EBL7207053 035 $a(CKB)26183512800041 035 $a(DE-He213)978-3-031-22580-2 035 $a(PPN)268205175 035 $a(EXLCZ)9926183512800041 100 $a20230522d2023 uy 0 101 0 $aeng 135 $aurcnu|||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 00$aSmart morphing and sensing for aeronautical configurations $eprototypes, experimental and numerical findings from the H2020 N° 723402 SMS EU project /$fMarianna Braza [and four others], editors 205 $a1st ed. 2023. 210 1$aCham, Switzerland :$cSpringer,$d[2023] 210 4$d©2023 215 $a1 online resource (287 pages) 225 1 $aNotes on numerical fluid mechanics and multidisciplinary design ;$vVolume 153 311 08$aPrint version: Braza, Marianna Smart Morphing and Sensing for Aeronautical Configurations Cham : Springer International Publishing AG,c2023 9783031225796 320 $aIncludes bibliographical references. 327 $aPrototypes 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. 330 $aThis book reports on advanced strategies to design, modeling and testing morphing wings for aeronautical applications. Covering the major outcomes of the multidisciplinary project ?Smart Morphing & Sensing? (H2020 N° 723402 SMS), funded by the European Union between 2017 and 2020, it presents a complete set of theories and methods that have been used and developed to integrate novel electroactive actuators and sensors in wings, for the purpose of increasing their aerodynamic efficiency and attenuate vibrations and noise. Topics include: integrated aeroelastic design of morphing wings using high-fidelity computational fluid dynamics and structural mechanics, distributed sensing using a new generation of high-fidelity fiber optics sensors, and controller design by appropriate flight control commands. Further, the book reports on advanced experimental techniques to validate novel actuation and sensing systems on the built prototypes via wind tunnel tests at subsonic (take-off and landing) and transonic (cruise) speeds. All in all, this volume provides readers with extensive and timely information on research and developments of bioinspired aircraft wings. . 410 0$aNotes on numerical fluid mechanics and multidisciplinary design ;$vVolume 153. 606 $aAirplanes$xWings$xDesign and construction 606 $aAirplanes$xWings$xMathematical models 615 0$aAirplanes$xWings$xDesign and construction. 615 0$aAirplanes$xWings$xMathematical models. 676 $a629.1343 702 $aBraza$b Marianna 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910672441703321 996 $aSmart Morphing and Sensing for Aeronautical Configurations$93044737 997 $aUNINA