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Donato de Rosa
Donato de Rosa
Italian Aerospace Research Center
Bestätigte E-Mail-Adresse bei cira.it
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Zitiert von
Zitiert von
Jahr
Assessment of predictive capabilities for aerodynamic heating in hypersonic flow
D Knight, O Chazot, J Austin, MA Badr, G Candler, B Celik, D de Rosa, ...
Progress in Aerospace Sciences 90, 39-53, 2017
932017
Performance improvements of a regional aircraft by riblets and natural laminar flow
P Catalano, D de Rosa, B Mele, R Tognaccini, F Moens
Journal of Aircraft 57 (1), 29-40, 2020
222020
Effects of riblets on the performances of a regional aircraft configuration in NLF conditions
P Catalano, D de Rosa, B Mele, R Tognaccini, F Moens
2018 AIAA Aerospace Sciences Meeting, 1260, 2018
122018
Suction optimization on thick airfoil to trap vortices
RS Donelli, P Iannelli, E Iuliano, D De Rosa
Conference of Italian association of theoretical and applied mechanics, 2010
122010
Parametric investigation of a distributed propulsion system on a regional aircraft
D de Rosa, E Morales Tirado, G Mingione
Aerospace 9 (4), 176, 2022
112022
Computational analysis of shock wave boundary layer interactions in non-equilibrium hypersonic flow
G Pezzella, D de Rosa, R Donelli
20th AIAA International Space Planes and Hypersonic Systems and Technologies …, 2015
92015
Effect of body shape on riblets performance
B Mele, R Tognaccini, P Catalano, D de Rosa
Physical Review Fluids 5 (12), 124609, 2020
82020
Large Eddy Simulations and RANS models for airfoils at low Reynolds number.
P Catalano, D de Rosa
AIAA AVIATION 2020 FORUM, 2990, 2020
72020
Flap effectiveness appraisal for winged re-entry vehicles
D de Rosa, G Pezzella, RS Donelli, A Viviani
Acta Astronautica 122, 175-184, 2016
72016
Application of different Lagrangian Particle Tracking techniques for water impingement
F Petrosino, D De Rosa, G Mingione
IOP Conference Series: Materials Science and Engineering 1024 (1), 012011, 2021
42021
RANS simulations of transitional flow by γ model
D de Rosa, P Catalano
International Journal of Computational Fluid Dynamics 33 (10), 407-420, 2019
42019
The use of RANS approach for predicting transition
S Russo, D De Rosa, RS Donelli, C de Nicola
Aerotecnica Missili & Spazio 97, 145-152, 2018
42018
Numerical rebuilding of high and low enthalpy hypersonic flow test over a double wedge model
G Pezzella, D de Rosa, RS Catalano
Numerical Rebuilding of High and Low Enthalpy Hypersonic Flow Test Over a …, 2015
42015
Natural Laminar Flow Transonic Wing Design Applied to Future Innovative Green Regional Aircraft.
IS El Din, JL Godard, AM Rodde, F Moens, G Andreutti, D De Rosa, ...
3AF/CEAS Conference" Greener Aviation: Clean Sky breakthroughs and worldwide …, 2014
42014
Validation of intermittency model for transition prediction in a RANS flow solver
D de Rosa, P Catalano
2018 AIAA Aerospace Sciences Meeting, 1043, 2018
32018
Riblets: Ready for application on next generation aircrafts?
R Tognaccini, B Mele, GPR Catalano, D De Rosa, G Iuso, S Sedda, ...
Titolo volume non avvalorato, 1-12, 2016
32016
A CIRA 3D Ice Accretion Code for Multiple Cloud Conditions Simulations
D Cinquegrana, F D'Aniello, D de Rosa, A Carozza, P Catalano, ...
SAE Technical Paper, 2023
22023
Analysis of riblets performance in pressure gradient flow by large eddy simulation
B Mele, R Tognaccini, P Catalano, D De Rosa
AIAA Scitech 2020 Forum, 0031, 2020
22020
Design And Ground Testing For The Expert PL4/PL5'Natural And Roughness Induced Transition'
D Masutti, O Chazot, R Donelli, D de Rosa
7th European Symposium on Aerothermodynamics 692, 66, 2011
22011
Multi-Step Ice Accretion by Immersed Boundaries
D de Rosa, F Capizzano, D Cinquegrana
SAE Technical Paper, 2023
12023
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