Please use this identifier to cite or link to this item:
|Title:||Aeroelastic study of flexible flapping wings by a coupled lattice Boltzmann-finite element approach with immersed boundary method||Authors:||De Rosis, A.
|Journal:||JOURNAL OF FLUIDS AND STRUCTURES||Issue Date:||2014||URI:||http://hdl.handle.net/2607/29837||DOI:||10|
|Appears in Collections:||A1. Articolo in rivista|
Show full item record
checked on Jan 23, 2021
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.