| CLAE Project. H3NS: Code Development Verification and Validation G Ranuzzi, S Borreca CIRA-CF-06-1017, 2006 | 52* | 2006 |
| Hypersonic low-density aerothermodynamics of Orion-like exploration vehicle R Votta, A Schettino, G Ranuzzi, S Borrelli Journal of Spacecraft and Rockets 46 (4), 781-787, 2009 | 33 | 2009 |
| Numerical investigation of a N2O-paraffin hybrid rocket engine combusting flowfield G Ranuzzi, D Cardillo, M Invigorito 6th european conference for aeronautics and space sciences (EUCASS), 2015 | 27 | 2015 |
| Numerical Prediction of Aerothermodynamic Effects on a Reentry Vehicle Body Flap Configuration M Di Clemente, M Marini, S Di Benedetto, A Schettino, G Ranuzzi IAC-2006, IAC-06-D2.6.08, 2006 | 27 | 2006 |
| Shock-wave/turbulent boundary-layer interactions in nonequilibrium flows F Grasso, M Marini, G Ranuzzi, S Cuttica, B Chanetz AIAA journal 39 (11), 2131-2140, 2001 | 27 | 2001 |
| Experimental and numerical investigation of aerothermal characteristics of hypersonic intermediate experimental vehicle P Roncioni, G Ranuzzi, M Marini, S Paris, E Cosson, T Walloschek Journal of Spacecraft and Rockets 48 (2), 291-302, 2011 | 24 | 2011 |
| Application of OpenFOAM for rocket design M Invigorito, D Cardillo, G Ranuzzi 9th OpenFOAM® Workshop, 1-15, 2014 | 14 | 2014 |
| Evaluation of Local Effects of Transitional Knudsen Number on Shock Wave Boundary Layer Interactions R Votta, G Ranuzzi, M Di Clemente, A Schettino, M Marini Wind Tunnels and Experimental Fluid Dynamics Research, 537-552, 2011 | 9* | 2011 |
| A CFD Method for Simulation of Mixing and Combustion in High-Pressure LOx Methane Rocket Engines L Cutrone, F Battista, G Ranuzzi, S Bonifacio, J Steelant 46th AIAA Aerospace Sciences Meeting and Exhibit. Jan 7 – 10, 2008, Reno, Nevada, 2008 | 9 | 2008 |
| Hypersonic CFD Characterization of IXV Vehicle P Roncioni, G Ranuzzi, M Marini, E Cosson Proceedings of the West-East High Speed Flow Field Conference, 2007 | 9 | 2007 |
| Numerical investigation of rocket engine combusting flowfields G Ranuzzi, L Cutrone, D Cardillo, M Invigorito 54th AIAA Aerospace Sciences Meeting, 2147, 2016 | 7 | 2016 |
| Rarefied Aerothermodynamics Technology Development for Future High-Altitude High-Speed Transport (EU-FAST20XX) R Votta, M Marini, G Ranuzzi, T Schlegat, K Hannemann, ... AIAA SPACE 2013 Conference and Exposition, 5330, 2013 | 7 | 2013 |
| Hybrid rocket technology in the frame of the italian HYPROB program M Di Clemente, R Votta, G Ranuzzi, F Ferrigno ESA 8th European Symposium on ATD for Space Vehicles, 2015 | 6 | 2015 |
| CFD aerothermodynamic characterization of the IXV hypersonic vehicle P Roncioni, G Ranuzzi, M Marini, F Battista, GC Rufolo 7th European symposium on aerothermodynamics of space vehicles, 9-12, 2011 | 6 | 2011 |
| Supersonic Combustion Models Application in Advanced Propulsion Concepts F Battista, L Cutrone, G Ranuzzi, S Borreca 15th AIAA International Space Planes and Hypersonic Systems and Technologies …, 2008 | 6 | 2008 |
| Injection system design of an N2O-paraffin hybrid rocket demonstrator G Elia, M Invigorito, M Di Clemente, R Votta, G Ranuzzi Young International Conference, Aachen, Germany, 2015 | 5 | 2015 |
| Numerical prediction of nozzle ablation in hybrid rocket engine M Panelli, D Cardillo, M Di Clemente, G Ranuzzi 6th EUCASS 29, 2015 | 5 | 2015 |
| Numerical and Experimental Analysis of Low-Density Effects in Suborbital Flight of FAST20XX R Votta, G Ranuzzi, M Marini, L Morsa, G Fels, T Schlegat, K Hannemann 43rd AIAA Thermophysics Conference, 2012 | 5 | 2012 |
| SPREAD: a Scramjet PREliminary Aerothermodynamic Design Code S Bonifacio, S Borreca, G Ranuzzi, V Salvatore 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, 2006 | 5 | 2006 |
| Real Gas Effects on a Planetary Re-entry Capsule S Bisceglia, G Ranuzzi AIAA/CIRA 13th International Space Planes and Hypersonics Systems and …, 2005 | 5 | 2005 |
Francesco BattistaCIRA, italian aerospace research centerVerified email at cira.it
