Roberto Albertani, Ph.D.
Affiliations: | 2005 | University of Florida, Gainesville, Gainesville, FL, United States |
Area:
Aerospace Engineering, Mechanical EngineeringGoogle:
"Roberto Albertani"Parents
Sign in to add mentorPeter G. Ifju | grad student | 2005 | UF Gainesville | |
(Experimental aerodynamic and static elastic deformation characterization of low aspect ratio flexible fixed wings applied to micro aerial vehicles.) |
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Publications
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Hu C, Albertani R. (2020) Machine learning applied to wind turbine blades impact detection Wind Engineering. 44: 325-338 |
Hu C, Albertani R, Suryan RM. (2018) Wind turbine sensor array for monitoring avian and bat collisions Wind Energy. 21: 255-263 |
Alioli M, Masarati P, Morandini M, et al. (2017) Membrane Shape and Load Reconstruction from Measurements Using Inverse Finite Element Analysis Aiaa Journal. 55: 297-308 |
Alioli M, Masarati P, Morandini M, et al. (2017) Modeling effects of membrane tension on dynamic stall for thin membrane wings Aerospace Science and Technology. 69: 419-431 |
Carpenter TJ, Albertani R. (2015) Aerodynamic Load Estimation from Virtual Strain Sensors for a Pliant Membrane Wing Aiaa Journal. 53: 2069-2079 |
Stanford B, Albertani R, Lacore D, et al. (2013) Proper Orthogonal Decomposition of Flexible Clap and Fling Elastic Motions via High-Speed Deformation Measurements Experimental Mechanics. 53: 1127-1141 |
Babcock J, Albertani R, Abate G. (2012) Experimental estimation of the rotary damping coefficients of a pliant wing Journal of Aircraft. 49: 390-397 |
Chakravarty UK, Albertani R. (2012) Experimental and finite element modal analysis of a pliant elastic membrane for micro air vehicles applications Journal of Applied Mechanics, Transactions Asme. 79 |
Chakravarty UK, Albertani R. (2011) Modal analysis of a flexible membrane wing of micro air vehicles Journal of Aircraft. 48: 1960-1967 |
Reich GW, Eastep FE, Altman A, et al. (2011) Transient poststall aerodynamic modeling for extreme maneuvers in micro air vehicles Journal of Aircraft. 48: 403-411 |