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Marco Di Clemente
Marco Di Clemente
aerospace engineer, CIRA
Email verificata su cira.it
Titolo
Citata da
Citata da
Anno
Design and development of a LOX/LCH4 technology demonstrator
V Salvatore, F Battista, R Votta, M Di Clemente, M Ferraiuolo, P Roncioni, ...
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 3935, 2012
302012
Numerical prediction of aerothermodynamic effects on a re-entry vehicle body flap configuration
M Di Clemente, M Marini, S Di Benedetto, A Schettino, G Ranuzzi
Acta Astronautica 65 (1-2), 221-239, 2009
252009
Aerodynamic and aerothermodynamic data base of Expert capsule
A Schettino, R Votta, P Roncioni, M Di Clemente, M Gerritsma, C Chiarelli, ...
Proceedings of the west-east high speed flow field conference, 19-22, 2007
192007
Development of a LOX/LCH4 Technology Demonstrator Based on Regenerative Cooling throughout Validation of Critical Design Aspects with Breadboards in the Framework of the Hyprob …
F Battista, M Di Clemente, M Ferraiuolo, R Votta, D Ricci, M Panelli, ...
63rd International Astronautical Congress, Naples, Italy. IAC-2012, 2012
162012
Hypersonic test analysis by means of aerothermal coupling methodology and infrared thermography
M Di Clemente, G Rufolo, A Ianiro, G Cardone
AIAA journal 51 (7), 1755-1769, 2013
152013
Shock Wave Boundary Layer Interaction in EXPERT Flight Conditions and" Scirocco" PWT
M Di Clemente, M Marini, A Schettino
AIAA/CIRA 13th International Space Planes and Hypersonics Systems and …, 2005
122005
CFD modelling and simulations of the HYPROB regenerative LOX/CH4 thrust chamber
P Roncioni, D Cardillo, M Panelli, D Ricci, M Di Clemente, F Battista
5th European Conference For Aeronautics And Space Sciences (EUCASS), 2013
112013
Test design methodologies for flight relevant plasma wind tunnel experiments
M Marini, S Di Benedetto, G Rufolo, M Di Clemente, S Borrelli
Invited Lecture at West-East High Speed Flow Field WEHSFF-2007 Conference …, 2007
112007
Evaluation of local effects of transitional Knudsen number on shock wave boundary layer interactions
R Votta, G Ranuzzi, A Schettino, M Marini
39th AIAA Thermophysics Conference, 4545, 2007
92007
Aerothermal Environment Definition for a Reusable Experimental Reentry Vehicle Wing Leading Edge
F Battista, GC Rufolo, M Di Clemente
46th AIAA Thermophysics Conference Miami AIAA 4048, 2007
72007
Plasma Wind Tunnel Test Design Methodologies for Re-entry Vehicle Components
S Di Benedetto, M Di Clemente, M Marini
2nd European Conference for Aerospace Sciences (EUCASS), 2007
72007
Aerothermal Enviroment Definition for a Reusable Experimental Re-Entry Vehicle Wing
F Battista, G Rufolo, M Di Clemente
39th AIAA Thermophysics Conference, 4048, 2007
72007
Numerical investigation of RCS jet interaction and plume impingement for Mars precision landing
R Votta, E Trifoni, G Pezzella, M Di Clemente, A Schettino, V Mareschi, ...
8th AIAA Theoretical Fluid Mechanics Conference, 3350, 2017
62017
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
62015
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
52015
Numerical prediction of nozzle ablation in hybrid rocket engine
M Panelli, D Cardillo, M Di Clemente, G Ranuzzi
6th EUCASS 29, 2015
52015
An extrapolation from flight methodology for a re-entry vehicle wing leading edge test in a plasma wind tunnel facility
M Di Clemente, G Rufolo, F Battista
39th AIAA Thermophysics Conference, 3895, 2007
52007
Shock Wave Boundary Layer Interactions in SCIROCCO Plasma Wind Tunnel
M Di Clemente, M Marini, A Schettino
East West High Speed Flow Field Conference, Beijing, China, 19-22, 2005
52005
Aeroshape trade-off and aerodynamic analysis of the space-rider vehicle
M Marini, M Di Clemente, G Guidotti, G Rufolo, O Lambert, N Joiner, ...
7th European Conference for Aeronautics and Space Sciences (EUCASS), 20, 2017
42017
A new global approach to evaluate the surface catalytic efficiency of tps materials based on arc jet experiments and numerical predictions
E Trifoni, S Di Benedetto, M Di Clemente
8th European Symposium on Aerothermodynamics for Space Vehicles, 2015
42015
Il sistema al momento non può eseguire l'operazione. Riprova più tardi.
Articoli 1–20