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Michele Ferlauto
Michele Ferlauto
Professor (associate), DIMEAS, Politecnico di Torino
Verified email at polito.it - Homepage
Title
Cited by
Cited by
Year
Numerical investigation of the dynamic characteristics of a dual-throat-nozzle for fluidic thrust-vectoring
M Ferlauto, R Marsilio
AIAA Journal 55 (1), 86-98, 2017
532017
An aerodynamic optimization method based on the inverse problem adjoint equations
A Iollo, M Ferlauto, L Zannetti
Journal of Computational Physics 173 (1), 87-115, 2001
532001
Numerical simulation of fluidic thrust-vectoring
M Ferlauto, R Marsilio
Aerotecnica Missili & Spazio 95, 153-162, 2016
312016
Time-marching throughflow analysis of multistage axial compressors based on a novel inviscid blade force model
C Yang, H Wu, J Yang, M Ferlauto
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2019
292019
Set of boundary conditions for aerodynamic design
M Ferlauto, A Iollo, L Zannetti
AIAA journal 42 (8), 1582-1592, 2004
192004
Differential throttling and fluidic thrust vectoring in a linear aerospike
M Ferlauto, A Ferrero, M Marsicovetere, R Marsilio
International Journal of Turbomachinery, Propulsion and Power 6 (2), 8, 2021
172021
The clean sky 2 midas project-an innovative modular, digital and integrated air data system for fly-by-wire applications
A Lerro, M Battipede, P Gili, M Ferlauto, A Brandl, A Merlone, ...
2019 IEEE 5th International Workshop on Metrology for AeroSpace …, 2019
162019
Reduced order modelling of full-span rotating stall for the flow control simulation of axial compressors
M Ferlauto, SR Taddei
Proceedings of the Institution of Mechanical Engineers, Part A: Journal of …, 2015
162015
A viscous inverse method for aerodynamic design
M Ferlauto, R Marsilio
Computers & fluids 35 (3), 304-325, 2006
162006
Open and closed-loop responses of a dual-throat nozzle during fluidic thrust vectoring
M Ferlauto, R Marsilio
52nd AIAA/SAE/ASEE Joint Propulsion Conference, 4504, 2016
152016
An inverse method of designing the cooling passages of turbine blades based on the heat adjoint equation
M Ferlauto
Proceedings of the Institution of Mechanical Engineers, Part A: Journal of …, 2014
152014
Thrust vectoring of a fixed axisymmetric supersonic nozzle using the shock-vector control method
E Resta, R Marsilio, M Ferlauto
Fluids 6 (12), 441, 2021
142021
Numerical simulation of the unsteady flowfield in complete propulsion systems
M Ferlauto, R Marsilio
Advances in Aircraft and Spacecraft Science 5 (3), 349-362, 2018
142018
A computational approach to the simulation of controlled flows by synthetic jets actuators
M Ferlauto, R Marsilio
Advances in aircraft and spacecraft science 2 (1), 77, 2015
142015
A numerical method for the study of fluidic thrust-vectoring
M Ferlauto, R Marsilio
Advances in aircraft and spacecraft science 3 (4), 367, 2016
132016
A pseudo-compressibility method for solving inverse problems based on the 3D incompressible Euler equations
M Ferlauto
Inverse Problems in Science and Engineering 23 (5), 798-817, 2015
132015
Point vortex model for asymmetric inviscid wakes past bluff bodies
A Elcrat, M Ferlauto, L Zannetti
Fluid Dynamics Research 46 (3), 031407, 2014
132014
Integrated design and analysis of intakes and nozzles in air-breathing engines
M Ferlauto, F Larocca, L Zannetti
Journal of propulsion and power 18 (1), 28-34, 2002
132002
Computational investigation of injection effects on shock vector control performance
M Ferlauto, R Marsilio
2018 Joint Propulsion Conference, 4934, 2018
122018
Numerical study of secondary mass flow modulation in a Bypass Dual-Throat Nozzle
MH Hamedi-Estakhrsar, M Ferlauto, H Mahdavy-Moghaddam
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2021
102021
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