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Annafederica Urbano
Annafederica Urbano
ISAE-SUPAERO
Verified email at isae-supaero.fr
Title
Cited by
Cited by
Year
Exploration of combustion instability triggering using large eddy simulation of a multiple injector liquid rocket engine
A Urbano, L Selle, G Staffelbach, B Cuenot, T Schmitt, S Ducruix, ...
Combustion and Flame 169, 129-140, 2016
2312016
Numerical analysis of deterioration in heat transfer to near-critical rocket propellants
M Pizzarelli, A Urbano, F Nasuti
Numerical Heat Transfer, Part A: Applications 57 (5), 297-314, 2010
1212010
Direct numerical simulation of nucleate boiling in micro-layer regime
A Urbano, S Tanguy, G Huber, C Colin
International Journal of Heat and Mass Transfer 123, 1128-1137, 2018
992018
Onset of heat transfer deterioration in supercritical methane flow channels
A Urbano, F Nasuti
Journal of Thermophysics and Heat Transfer 27 (2), 298-308, 2013
882013
Study of flame response to transverse acoustic modes from the LES of a 42-injector rocket engine
A Urbano, Q Douasbin, L Selle, G Staffelbach, B Cuenot, T Schmitt, ...
Proceedings of the Combustion Institute 36 (2), 2633-2639, 2017
682017
Parametric analysis of heat transfer to supercritical-pressure methane
A Urbano, F Nasuti
Journal of Thermophysics and Heat Transfer 26 (3), 450-463, 2012
512012
Conditions for the occurrence of heat transfer deterioration in light hydrocarbons flows
A Urbano, F Nasuti
International Journal of Heat and Mass Transfer 65, 599-609, 2013
502013
Direct numerical simulation of nucleate boiling in zero gravity conditions
A Urbano, S Tanguy, C Colin
International Journal of Heat and Mass Transfer 143, 118521, 2019
292019
Parametric analysis of cooling properties of candidate expander-cycle fuels
A Urbano, F Nasuti
Journal of Propulsion and Power 30 (1), 153-163, 2014
232014
Driving and damping mechanisms for transverse combustion instabilities in liquid rocket engines
A Urbano, L Selle
Journal of Fluid Mechanics 820, R2, 2017
192017
Numerical analysis of transcritical fluids heating in liquid rocket engine cooling channels
A Urbano, M Pizzarelli, F Nasuti
The Journal of Aerospace Science Technology Systems 88 (1/2), 20-30, 2009
182009
A semi implicit compressible solver for two-phase flows of real fluids
A Urbano, M Bibal, S Tanguy
Journal of Computational Physics 456, 111034, 2022
172022
Coaxial-injector surrogate modeling based on Reynolds-averaged Navier–Stokes simulations using deep learning
M Krügener, JF Zapata Usandivaras, M Bauerheim, A Urbano
Journal of Propulsion and Power 38 (5), 783-798, 2022
142022
CFD analysis of hybrid rocket flowfields including fuel pyrolysis and nozzle ablation
D Bianchi, F Nasuti
49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, 3637, 2013
142013
Numerical analysis of heated channel flows by a space-marching finite volume technique
A Urbano, F Nasuti
Journal of Thermophysics and Heat Transfer 25 (2), 282-290, 2011
142011
On the coupling between direct numerical simulation of nucleate boiling and a micro-region model at the contact line
L Torres, A Urbano, C Colin, S Tanguy
Journal of Computational Physics 497, 112602, 2024
102024
Numerical study of liquefied natural gas as a coolant in liquid rocket engines
A Urbano, F Nasuti
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2013
102013
Thermoacoustic feedback analysis of a cylindrical combustion chamber under supercritical conditions
M Schulze, A Urbano, M Zahn, M Schmid, T Sattelmayer, M Oschwald
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 3776, 2014
92014
Data driven models for the design of rocket injector elements
JF Zapata Usandivaras, A Urbano, M Bauerheim, B Cuenot
Aerospace 9 (10), 594, 2022
62022
An approximate Riemann solver for real gas parabolized Navier–Stokes equations
A Urbano, F Nasuti
Journal of Computational Physics 233, 574-591, 2013
62013
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