Print Email Facebook Twitter Coupled Nonlinear Aeroelasticity and Flight Dynamics for Stability Analysis of Flexible Wing Structures Title Coupled Nonlinear Aeroelasticity and Flight Dynamics for Stability Analysis of Flexible Wing Structures Author Natella, M. Contributor De Breuker, R. (mentor) Werter, N.P.M. (mentor) Faculty Aerospace Engineering Department ASCM Date 2015-12-11 Abstract The present work thus develops a low-fidelity formulation to investigate the flight dynamic stability of a flexible wing structure. The model is verified against other studies found in the relevant literature, which show interesting trends in terms of how some of the design variables or flight conditions influence the stability of the structure. Subject aeroelasticityflight dynamicsflexible wingsstability analysis To reference this document use: http://resolver.tudelft.nl/uuid:39984220-1d55-43fb-b42c-8a692a979211 Part of collection Student theses Document type master thesis Rights (c) 2015 Natella, M. Files PDF MscThesis_MarioNatella.pdf 1.95 MB Close viewer /islandora/object/uuid:39984220-1d55-43fb-b42c-8a692a979211/datastream/OBJ/view