Annafederica Urbano
Annafederica Urbano
ISAE-SUPAERO
E-mailová adresa ověřena na: isae-supaero.fr
Název
Citace
Citace
Rok
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
1262016
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
952010
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
572013
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
402017
Parametric analysis of heat transfer to supercritical-pressure methane
A Urbano, F Nasuti
Journal of Thermophysics and Heat Transfer 26 (3), 450-463, 2012
402012
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
332013
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
322018
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
162009
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
Parametric analysis of cooling properties of candidate expander-cycle fuels
A Urbano, F Nasuti
Journal of Propulsion and Power 30 (1), 153-163, 2014
122014
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
122013
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
72019
Driving and damping mechanisms for transverse combustion instabilities in liquid rocket engines
A Urbano, L Selle
Journal of Fluid Mechanics 820, pp. 820 R2/1-820 R2/12, 2017
72017
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
72014
An approximate Riemann solver for real gas parabolized Navier–Stokes equations
A Urbano, F Nasuti
Journal of Computational Physics 233, 574-591, 2013
52013
Analysis of coaxial-flame response during transverse combustion instability
A Urbano, Q Douasbin, L Selle
7th EUCASS. Milano, Italy, 2017
42017
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
32013
Investigations on Thermoacoustic Feedback on a Representative Test Chamber Configuration
A Urbano, M Schulze, M Zahn, M Schmid, T Sattelmayer, M Oschwald
Proceedings of the Summer Program, Sonderforschungsbereich Transregio 40, 2013
32013
Analysis of Heat Transfer Characteristics of Supercritical Fuels in Rocket Cooling Systems by a Space Marching Numerical Technique
A URBANO
32012
Joint experimental, les and helmholtz analysis of self-excited combustion instabilities in a hydrogen-oxygen rocket combustor
Q Douasbin, S Gröning, A Urbano, L Selle, J Hardi, W Armbruster, ...
22016
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Články 1–20