Aeroelastic study of flexible flapping wings by a coupled lattice Boltzmann-finite element approach with immersed boundary method

Author(s)
De Rosis, A.
Falcucci, G.
Ubertini, F.
Date Issued
2014
Type
article
Volume
49
Issue
49
Start Page
516
End Page
533
DOI
ISSN
8899746
Journal
Handle
Conference(s)
JOURNAL OF FLUIDS AND STRUCTURES