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Flexible engineering toward green ai...

Biancolini, Marco Evangelos.

Flexible engineering toward green aircraftCAE tools for sustainable mobility /

Record Type:	Electronic resources : Monograph/item
Title/Author:	Flexible engineering toward green aircraftedited by Marco Evangelos Biancolini, Ubaldo Cella.
Reminder of title:	CAE tools for sustainable mobility /
other author:	Biancolini, Marco Evangelos.
Published:	Cham :Springer International Publishing :2020.
Description:	xii, 187 p. :ill., digital ;24 cm.
Contained By:	Springer eBooks
Subject:	Aerospace engineering.
Online resource:	https://doi.org/10.1007/978-3-030-36514-1
ISBN:	9783030365141$q(electronic bk.)

Flexible engineering toward green aircraftCAE tools for sustainable mobility /
Flexible engineering toward green aircraftCAE tools for sustainable mobility /[electronic resource] :edited by Marco Evangelos Biancolini, Ubaldo Cella. - Cham :Springer International Publishing :2020. - xii, 187 p. :ill., digital ;24 cm. - Lecture notes in applied and computational mechanics,v.921613-7736 ;. - Lecture notes in applied and computational mechanics ;v.61..

The next generation of aircraft -- Aeroelastic wind tunnel tests of the RIBES wing model -- Validation of high fidelity computational methods for aeronautical FSI analyses -- High-fidelity static aeroelastic simulations of the Common Research Model -- Aero-elastic simulations using the NSMB CFD solver including results for a Strut Braced Wing -- Semi-analytical modeling of non-stationary fluid-structure interaction -- Fluid structure modelling of ground induced vibrations by mesh morphing and modal superposition -- Unsteady FSI Analysis of a Square Array of Tubes in Water Crossflow -- Risk measures applied to robust aerodynamic shape design optimization -- Aero-structural Optimization of a MALE configuration in the AGILE MDO Framework.

This book discusses the recent advances in aircraft design methodologies. It provides an overview of topics such as shape optimization, robust design and aeroelasticity, focusing on fluid-structure numerical methodologies to address static and dynamic aeroelastic problems. It demonstrates that the capability to evaluate the interaction between aerodynamics, inertia and elastic forces is important to avoid drag penalties, control system efficiency loss and generation of potentially dangerous phenomena, such as divergence, control reversal and flutter. The book particularly highlights the advances in "high fidelity" CFD-CSM coupling, describing the latest experimental research to validate the numerical fluid-structure interaction analysis methodologies resulting from the EU-funded RBF4AERO and RIBES projects.

ISBN: 9783030365141$q(electronic bk.)

Standard No.: 10.1007/978-3-030-36514-1doiSubjects--Topical Terms:

324294
Aerospace engineering.

LC Class. No.: TL545 / .F549 2020

Dewey Class. No.: 629.1

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505 0 $a The next generation of aircraft -- Aeroelastic wind tunnel tests of the RIBES wing model -- Validation of high fidelity computational methods for aeronautical FSI analyses -- High-fidelity static aeroelastic simulations of the Common Research Model -- Aero-elastic simulations using the NSMB CFD solver including results for a Strut Braced Wing -- Semi-analytical modeling of non-stationary fluid-structure interaction -- Fluid structure modelling of ground induced vibrations by mesh morphing and modal superposition -- Unsteady FSI Analysis of a Square Array of Tubes in Water Crossflow -- Risk measures applied to robust aerodynamic shape design optimization -- Aero-structural Optimization of a MALE configuration in the AGILE MDO Framework.
520 $a This book discusses the recent advances in aircraft design methodologies. It provides an overview of topics such as shape optimization, robust design and aeroelasticity, focusing on fluid-structure numerical methodologies to address static and dynamic aeroelastic problems. It demonstrates that the capability to evaluate the interaction between aerodynamics, inertia and elastic forces is important to avoid drag penalties, control system efficiency loss and generation of potentially dangerous phenomena, such as divergence, control reversal and flutter. The book particularly highlights the advances in "high fidelity" CFD-CSM coupling, describing the latest experimental research to validate the numerical fluid-structure interaction analysis methodologies resulting from the EU-funded RBF4AERO and RIBES projects.
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