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.
Reihe
Sprache
Verlagsort
Verlagsgruppe
Springer International Publishing
Illustrationen
77
53 s/w Abbildungen, 77 farbige Abbildungen
XII, 187 p. 130 illus., 77 illus. in color.
Dateigröße
ISBN-13
978-3-030-36514-1 (9783030365141)
DOI
10.1007/978-3-030-36514-1
Schweitzer Klassifikation
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.
