Flávio J. Silvestre
Flávio J. Silvestre
Professor of Aeronautical Engineering
Verified email at
Cited by
Cited by
Formulation of the flight dynamics of flexible aircraft using general body axes
AB Guimaraes Neto, RGA Silva, P Paglione, FJ Silvestre
AIAA Journal 54 (11), 3516-3534, 2016
Aircraft control based on flexible aircraft dynamics
FJ Silvestre, AB Guimarães Neto, RM Bertolin, RGA da Silva, P Paglione
Journal of Aircraft 54 (1), 262-271, 2017
Experimental validation of a flight simulation model for slightly flexible aircraft
FJ Silvestre, R Luckner
AIAA Journal 53 (12), 3620-3636, 2015
Closed-loop control of a free shear flow: a framework using the parabolized stability equations
K Sasaki, G Tissot, AVG Cavalieri, FJ Silvestre, P Jordan, D Biau
Theoretical and Computational Fluid Dynamics 32 (6), 765-788, 2018
Dynamics and control of a flexible aircraft
F Silvestre, P Paglione
AIAA atmospheric flight mechanics conference and exhibit, 6876, 2008
Gust load alleviation in a flexible smart idealized wing
TSS Versiani, FJ Silvestre, ABG Neto, DA Rade, RGA da Silva, ...
Aerospace Science and technology 86, 762-774, 2019
Methodology for Modelling the Dynamics of Flexible, High-Aspect-Ratio Aircraft in the Time Domain for Aeroservoelastic Investigations
FJ Silvestre
mbv, Mensch-und-Buch-Verlag, 2013
Closed-loop control of wavepackets in a free shear-flow
K Sasaki, G Tissot, AV Cavalieri, FJ Silvestre, P Jordan, D Biau
22nd AIAA/CEAS Aeroacoustics Conference, 2758, 2016
Aeroelastic behavior of a composite plate-like wing under piezoelectrically induced stresses
TSS Versiani, DQ Tsunematsu, MV Donadon, FJ Silvestre, ABG Neto, ...
Mechanical Systems and Signal Processing 143, 106795, 2020
Active and passive control for acceleration reduction of an aeroelastic typical wing section
GC Silva, FJ Silvestre, MV Donadon, OS Santos, AB Guimaraes Neto, ...
Journal of Vibration and Control 24 (13), 2673-2687, 2018
Fuzzy gain-scheduling applied for a very flexible aircraft
GC Barbosa, R Bertolin, PJ González, AB Guimaraes Neto, FJ Silvestre
2018 AIAA Guidance, Navigation, and Control Conference, 1868, 2018
Experimental and numerical investigation of post-flutter limit cycle oscillations on a cantilevered flat plate
K Ramesh, TP Monteiro, FJ Silvestre, GN Antonio Bernardo, ...
Linear control of highly flexible aircraft based on loop separation
PJ Gonzalez, FJ Silvestre, P Paglione, A Köthe, ZY Pang, CE Cesnik
AIAA Atmospheric Flight Mechanics Conference, 3398, 2016
Equations of motion for optimal maneuvering with global aerodynamic model
MAV Morales, FJ Silvestre, ABG Neto
Aerospace Science and Technology 77, 206-216, 2018
aes Neto, G., de Souza Siqueria Versiani, T., and da Silva, RGA,“Experimental and Numerical Investigation of Post-Flutter Limit Cycle Oscillations on a Cantilevered Flat Plate,”
K Ramesh, TP Monteiro, FJ Silvestre, A Bernardo
International Forum on Aeroelasticity and Structural Dynamics 2017, 2017
Real-time reactive control of stochastic disturbances in forced turbulent jets
IA Maia, P Jordan, AVG Cavalieri, E Martini, K Sasaki, FJ Silvestre
Physical Review Fluids 6 (12), 123901, 2021
Experimental and numerical investigations on the nonlinear aeroelastic behavior of high aspect-ratio wings for different chord-wise store positions under stall and follower …
GC Silva, MV Donadon, FJ Silvestre
International Journal of Non-Linear Mechanics 131, 103685, 2021
Applicability of Geometrically-Linear Structural-Dynamic Models for the Flight Dynamics of Arbitrarily-Flexible Aircraft
ABG Neto, FL Cardoso-Ribeiro, FJ Silvestre
Belo Horizonte, Brazil), ICAS-31st Congress of the International Council of …, 2018
Evaluation of the impacts of objective function definition in aircraft conceptual design
DHB Di Bianchi, TH Orra, FJ Silvestre
Journal of Aircraft 55 (3), 1231-1243, 2018
Validity of the assumption of small deformations in aircraft with different levels of structural flexibility
AB Guimarães Neto, FJ Silvestre, FL Cardoso-Ribeiro, FLS Bussamra, ...
International Forum on Aeroelasticity and Structural Dynamics (IFASD), 2017
The system can't perform the operation now. Try again later.
Articles 1–20