giuseppe pezzella cv-itadidattica.cressi.unicampania.it/cv/057047-it.pdf · 2020. 8. 31. · (anno...

Curriculum Vitae Giuseppe Pezzella

© European Union, 2002-2018 | europass.cedefop.europa.eu / 14

INFORMAZIONI PERSONALI Giuseppe Pezzella

Departimento di Ingegneria.

[email protected]

http://www.diii.unina2.it/dipartimento/docenti-csa?MATRICOLA=057047

ESPERIENZA LAVORATIVA

Departimento di Ingegneria

Università della Campania “Luigi Vanvitelli”

www.unicampania.it

▪ Docente di Aerodinamica ed Aerotermodinamica dei Velivoli

(Nov 2018 – )

Laboratorio di Analisi ed Estrapolazione al Volo

Centro Italiano Ricerche Aerospaziali, CIRA

https://www.cira.it/

▪ Responsabile

(Febbraio 2015 – Nov 2018)

Ambito: Ricerca e Sviluppo nell’ambito dei flussi a bassa e alta velocità

erhAfbsdfbfefrherghergrrrherhirplane Aerodynamics

University of Campania “L. Vanvitelli”. Aversa (CE). Italy

http://www.diii.unina2.it

▪ Lecturer ▪

(Gen 2010 – Gen 2015)

Airplane Aerodynamics

Aerodinamica dei Velivoli

Università della Campania “L. Vanvitelli”. Aversa (CE). Italia

http://www.diii.unina2.it

▪ Docente a contratto

(Anno Accademico 2017 -2018)



Dipartimento Sistemi Spaziali


▪ Ricercatore, Specialista in Fluidodinamica

(Set. 2010 – Dicembre 2010)

Ambito: Ricerca e Sviluppo nell’ambito dei Sistemi Spaziali

Laboratorio di Aerotermodinamica


▪ Ricercatore

(Set. 2006 – Agosto 2010)

Ambito: Ricerca e Sviluppo nell’ambito dei flussi ad alta energia in non equilibrio termo-chimico

Laboratorio di Aerotermodinamica


▪ Ricercatore junior

(Mag 2005 – Aprile 2006)

Ambito: Ricerca e Sviluppo nell’ambito dei flussi ad alta energia in non equilibrio termo-chimico

Laboratorio di Dinamica dei Fluidi


▪ Ricercatore Senior

Ambito: Ricerca e Sviluppo nell’ambito dei flussi a bassa e alta velocità



EDUCAZIONE E FORMAZIONE

SKILLS PERSONALI

Revisore delle seguenti Riviste Scientifiche

� Aerospace Science and Technology. Elsevier

� Acta Astronautica. Elsevier

� Proceedings of the Institution of Mechanical Engineers, Part G, Journal of Aerospace Engineering; SAGE

Dipartimento di Scienza ed Ingegneria dello Spazio

Università degli Studi di Napoli “Federico II”. Napoli. Italia

▪ Ricercatore

(Aprile 2004 – Sett 2004)

Ambito: Ricerca e Sviluppo nell’ambito dei Sistemi Spaziali di Rientro

Dipartimento di Scienza ed Ingegneria dello Spazio


▪ Ricercatore

(Febbraio 2004 – Marzo 2004)

Ambito: Ricerca e Sviluppo nell’ambito della Meccanica del volo dei Sistemi Spaziali di Rientro

Master course: Experimental determination of Dynamic stability parameters

Von Karman Institute for Fluid Dynamics. Waterloosesteenweg 72 B-1640 Sint-Genesius-Rode

Belgio

(Febbraio 2008)

▪ Analisi della Stabilità Statica e Dinamica dei Veicoli Spaziali durante il Rientro Atmosferico

Master course: Research and Development for Airplane Design


(Sett. 2004 – Aprile 2005)

▪ Design Multidisciplinare dei Velivoli

Fundamentals of Hypersonics.

American Institute of Aeronautics and Astronautics (AIAA). Los Angeles. California. USA.

(Giugno 2001)

▪ Aerodinamica e Aerotermodinamica dei Velivoli di Rientro

Dottorato di Ricerca in Ingegneria Aerospaziale


(Sett 2000 – Dicembre 2003)

▪ Aerodinamica e Aerotermodinamica dei Velivoli di Rientro di Nuova Generazione

Laurea in Ingegneria Aeronautica Ind. Spaziale


(Sett 1992 – Giugno 1997)

Lingua Madre Italiano

COMPRENSIONE SPEAKING WRITING Altre lingue

Listening Reading Spoken interaction Spoken production

English B2 B2 B2 B2 B2



� Engineering Applications of Computational Fluid Mechanics

� Chinese Journal of Aeronautics (CJA). Elsevier

Pubblicazioni

Libri

Antonio Viviani and Giuseppe Pezzella, Next Generation Launchers Aerodynamics. Research Signpost, T.C. 37/661 (2), Fort P.O., Trivandrum-695 023. Kerala, India. ISBN: 978-81-308-0512-2

Capitoli in Libri

1. A. Viviani, G. Pezzella, “Computational Flowfield Analysis of a Planetary Entry Vehicle”. Book title: Numerical Simulations - Examples and Applications in Computational Fluid Dynamics. Published by In-Tech. Kirchengasse 43/3, A-1070 Vienna, Austria. Hosti 80b, 51000 Rijeka, Croatia. ISBN: 978-953-307-153-4.

2. E. Bucchignani, G. Pezzella, A. Matrone, “Numerical Simulation of Liquid-structure Interaction Problem in a Tank of a Space Re-entry Vehicle”. Book title: Numerical Simulations - Examples and Applications in Computational Fluid Dynamics. Published by In-Tech. Kirchengasse 43/3, A-1070 Vienna, Austria. Hosti 80b, 51000 Rijeka, Croatia. ISBN: 978-953-307-153-4.

3. G. Pezzella, “Aerodynamic Design of VTO-Hopper Vehicle of Future Launchers Preparatory Programme”. Book title: Fluid Dynamics / Book 2. Published by In-Tech. Kirchengasse 43/3, A-1070 Vienna, Austria. Hosti 80b, 51000 Rijeka, Croatia. ISBN: 979-953-307-631-6.

4. A. Viviani, G. Pezzella, “Fluid Dynamics Analysis of a Space Vehicle entering the Mars Atmosphere”. Book title: Fluid Dynamics/Book 2. Published by In-Tech. Kirchengasse 43/3, A-1070 Vienna, Austria. Hosti 80b, 51000 Rijeka, Croatia. ISBN: 979-953-307-631-6.

5. A. Viviani, L. Savino, G. Pezzella, “Dependence and Sensitivity on the Aerothermochemical Model of Atmospheric Re-entry Trajectories”. Book title: Progress in Flight Physics Volume 3. EUCASS Book Series. ISBN: 978-2-7598-0674-4. http://dx.doi.org/10.1051/eucass/201203253

6. A. Viviani, G. Pezzella, “Non-Equilibrium Computational Flowfield Analysis for the Design of Mars Manned Entry Vehicles”. Book title: EUCASS Flight Physics Book (Volume 5). ISBN: 978-2-7598-0877-9

7. A. Viviani, G. Pezzella, “Aerodynamics and Aerothermodynamics Assessment of a Mars Sample Return Mission”. Book title: Mars: Evolution, Geology and Exploration. Nova Publisher, New York. ISBN: 978-1-62618-102-1

8. G. Pezzella, A. Viviani, “Overview of Design Analysis of a Space Mission for Sample Returning from Mars”. Book title: Mars: Evolution, Geology and Exploration. Nova Publisher, New York. ISBN: 978-1-62618-102-1

9. G. Pezzella, A. Viviani, “Aerodynamic Performance Analysis of Three Different Unmanned Re-entry Vehicles”. Book title: Advanced UAV Aerodynamics, Flight Stability and Control: Novel Concepts, Theory and Applications. DOI: 10.1002/9781118928691.ch3 © 2017 John Wiley & Sons Ltd.

10. G. Pezzella, A. Viviani, “Launcher Aerodynamics: a Suitable Investigation Approach at Phase-A Design Level”. Book title: Advances in Hypersonic Vehicles Technologies. Published by In-Tech. Kirchengasse 43/3, A-1070 Vienna, Austria. Hosti 80b, 51000 Rijeka, Croatia. DOI: 10.5772/intechopen.68209. ISBN: 978-953-51-3904-1. Print ISBN: 978-953-51-3903-4.

11. G. Pezzella, “An Aerothermal Analysis of an Engine Nacelle for a General Aviation Airplane Model”. Book title: Advances in Engineering Research. Volume 20. Nova Science Publisher, Inc. New York. ISBN: 978-1-53612-992-2 (eBook). ISSN: 2163-3932



Riviste

1. R. Savino, G. Pezzella, “Numerical Analysis of Supersonic Combustion Ram-Jet with Upstream Fuel Injection”. International Journal for Numerical Method in Fluids 2003; 43:165-181. John Wiley & Sons, Ltd.

2. R. Monti, G. Pezzella, “A New Philosophy for the Design of Re-Entry Vehicles”, Special Issue of Space Technology on Advanced re-entry vehicles. 24-3. August 2004. Lister Science.

3. G. Pezzella, M. Marini, P. Roncioni, J. Kauffmann, C. Tomatis, “Preliminary Design of Vertical Takeoff Hopper Concept of Future Launchers Preparatory Program”, Journal of Spacecraft and Rockets 2009. ISSN 0022-4650 vol.46 no.4 (788-799) doi: 10.2514/1.39193

4. A. Viviani, G. Pezzella, “Nonequilibrium Aerothermodynamics of Capsule Reentry Vehicle”, Engineering Applications of Computational Fluid Mechanics Vol.3, No.4, pp.543-561 (2009). ISSN 1994-2060.

5. A. Viviani, G. Pezzella, “Heat Transfer Analysis for a Winged Reentry Flight Test Bed”, International Journal of Engineering (IJE), Volume (3): Issue (3). 2009. ISSN (Online): 1985-2312. www.cscjournals.org/csc/manuscript/Journals/IJE/.../IJE-85.pdf

6. A. Viviani, G. Pezzella, “Computational Flowfield Analysis over a Blunt-Body Reentry Vehicle”, Journal of Spacecraft and Rockets 2010. ISSN 0022-4650 vol.47 no.2 (258-270) doi: 10.2514/1.40876

7. E. Bucchignani, G. Pezzella, “Computational Flowfield Analyses of hypersonic Problems with Reacting Boundary Layer”. Mathematics and Computers in Simulation, ISSN 0378-4754 vol.81 no.3 (656-669). doi:10.1016/j.matcom.2010.01.003.

8. G. Pezzella, M. Marini, P. De Matteis, J. Kauffmann, A. Dapra and C. Tomatis, “Aerothermodynamic Analyses of Four Reusable Launchers in the Framework of ESA Future Launchers Preparatory Programme”. Aerotecnica Missili & Spazio (The Journal of Aerospace Science, Technologies & Systems). Vol. 89 No. 1 January 2010.

www.aidaa.it/1-2010/articolo_4.pdf

9. A. Viviani, G. Pezzella, C. Golia, “Effects of Thermochemical Modelling and Surface Catalyticity on an Earth Re-Entry Vehicle”, Proceedings of the Institution of Mechanical Engineers, Part G, Journal of Aerospace Engineering. 2010. Issue 5 (May), vol. 225. ISSN: 0954-4100 (Print) 2041-3025 (Online). doi 10.1177/2041302510392875. Sage Publications. Pag.1-18.

10. G. Pezzella, A. Viviani, “Aerodynamic Analysis of a Manned Space Vehicle for Missions to Mars”, Journal of Thermodynamics. vol. 2011, Article ID 857061, 13 pages, doi:10.1155/2011/857061. ISSN:1687-9244. e-ISSN:1687-9252 doi:10.1155/JTD. http://downloads.hindawi.com/journals/jtd/2011/857061.pdf

11. G. Pezzella, E. Bucchignani, “Numerical Assessment of the Flowfield Features at the Exit of SCIROCCO Plasma Wind Tunnel Nozzle”. Mathematics and Computers in Simulation, ISSN 0378-4754 vol.82 no.1 (118-131). doi:10.1016/j.matcom.2011.01.010.

12. G. Pezzella, “Aerodynamic and Aerothermodynamic Trade-off Analysis of a Small Hypersonic Flying Test Bed”. Acta Astronautica, doi:10.1016/j.actaastro.2011.03.004. Volume (69): Issue (3-4). 2011. ISSN (0094-5765): pag. 209-222.

13. G. Pezzella, “Preliminary Aerodynamic and Aerothermodynamic Assessment of the VTO Hopper Booster”. ISRN Mechanical Engineering. Volume 2011 (2011), Article ID 215785, 15 pages. doi:10.5402/2011/215785.

14. G. Pezzella, A. Viviani, “Aerodynamic Analysis of a Manned Mars Exploration Capsule”. Acta Astronautica, doi:10.1016/j.actaastro.2011.06.020 . Volume (69): Issue (11-12). 2011. ISSN (0094-5765): pag. 975-986.

15. G. Pezzella, “Aerodynamic and Aerothermodynamic design of Future Launchers Preparatory Program Concepts”. Aerospace Science and Technology, Volume 23, Issue 1, December 2012, Pages 233–249. http://dx.doi.org/10.1016/j.ast.2011.07.011.

16. G. Pezzella, “Hypersonic Aerothermal Environment Assessment of the CIRA FTB-X Reentry Vehicle”. Aerospace Science and Technology, Volume 25, Issue 1, March 2013, Pages 190-202.



http://dx.doi.org/10.1016/j.ast.2012.01.007.

17. G. Pezzella, “Ablative Heatshield Design for a Sample Return Vehicle”. Journal of Spacecraft Exploration. 2 (1) pag. (52-64). Print: ΙSSΝ: 2319.9814, Οn line: ΙSSΝ: 2319.9822.

18. G. Pezzella, G. Marino, G. Rufolo, “Aerodynamic Database Development of the ESA Intermediate Experimental Vehicle”. Acta Astronautica, DOI:10.1016/j.actaastro.2013.07.019. Volume (94). Issue (1). January–February 2014. ISSN (0094-5765): pag. (57–72).

19. G. Pezzella, “Assessment of the Aerodynamic and Aerothermodynamic Performance of a High-Lift Re-entry Vehicle”. Advances in Aircraft and Spacecraft Science, An International Journal. Vol. 2, No.2, April, 2015. pages 109-124. DOI: 10.12989/aas.2015.2.2.109.

20. G. Pezzella, E. Trifoni, “Aerodynamic and Aerothermodynamic Analysis of High Speed Earth Re-Entry Capsule”, Int. J. Aerodynamics, in press (Vol. 5, No. 1, 2015). https://doi.org/10.1504/IJAD.2015.074623

21. D. Cinquegrana, G. Pezzella, P. Catalano, “Aerodynamic and Aerothermodynamic Design of the USV3 Re-Entry Vehicle”. Aerotecnica Missili & Spazio (The Journal of Aerospace Science, Technologies & Systems).Vol 94. No 3. (2015).

22. M. Musto, N. Bianco, G. Rotondo, F. Toscano, G. Pezzella, “A simplified methodology to simulate a heat exchanger in an aircraft's oil cooler by means of a Porous Media model”. Applied Thermal Engineering 94 (2016) 836–845. Elsevier. http://dx.doi.org/10.1016/j.applthermaleng.2015.10.147

23. D. de Rosa, G. Pezzella, R. S. Donelli, A. Viviani. “Flap Effectiveness Appraisal for Winged Re-Entry Vehicles”. Acta Astronautica, DOI:10.1016/j.actaastro.2013.07.019. Volume 122, May–June 2016, Pages 175–184. doi:10.1016/j.actaastro.2015.12.052

24. G. Pezzella, A. Viviani, “Aerodynamic Performance Analysis of a Winged Re-Entry Vehicle From Hypersonic Down to Subsonic Speed”. Aerospace Science and Technology, Volume 52, March 2016, Pages 129-143. DOI information: 10.1016/j.ast.2016.02.030

25. D. Knight, O. Chazot, J. Austin, M. Ali Badr, G. Candler, B. Celik, D. de Rosa, R. Donelli, J. Komives, A. Lani, D. Levin, I. Nompelis, M. Panesi, G. Pezzella, B. Reimann, O. Tumuklu, K. Yuceil, “Assessment of predictive capabilities for aerodynamic heating in hypersonic flow”. Progress in Aerospace Sciences 90 (2017) 39–53. http://dx.doi.org/10.1016/j.paerosci.2017.02.001

26. F. Piscitelli, L. Cutrone, G. Pezzella, P. Roncioni, M. Marini, “Nose-to-tail analysis of an airbreathing hypersonic vehicle using an in-house simplified tool.”. Acta Astronautica, article in press. http://doi.org/10.1016/j.actaastro.2017.03.007

27. A. Viviani and G. Pezzella, “Aerodynamic Performance Analysis of Three Different Vehicle Concepts”. Aerotecnica Missili & Spazio (The Journal of Aerospace Science, Technologies & Systems). Vol 96, No 1 (2017). January-March 2017.

28. A. Carozza, G. Mingione, G. Pezzella, G. Serino, “Numerical investigation of the internal and external thermal fields for a nacelle in pusher configuration” Aerotecnica Missili & Spazio (The Journal of Aerospace Science, Technologies & Systems). Vol 96, No 1 (2017). January-March 2017.

29. N. Favaloro, M. P. Di Donato, A. Rispoli, G. Pezzella, “Preliminary analysis of the HEXAFLY-International Vehicle”. Vol 97, No 3 (2018). Pages 113-128. July-Sept 2018.

30. S. Di Giorgio, D. Quagliarella, G. Pezzella, S. Pirozzoli, “An aerothermodynamic design optimization framework for hypersonic vehicles”. Aerospace Science and Technology. Volume 84, January 2019, Pages 339-347.

NATO AVT

1. P. Hendrick, M. Gobeil & A. Morabito, Ch. Roba, A. Carozza, G. Mingione, G. Pezzella, Installation issues of a small turboshaft engine into a light helicopter. AVT-230 CSO_Paper 29_v1.

2. Assessment of Predictive Capabilities for Aerodynamic Heating of Hypersonic Systems AVT205-Final-



Report_v6

Proceedings a Congressi e Conferenze

1. R. Monti, R. Savino, G. Pezzella, D. Paterna, “Supersonic Combustion Ram-Jet Configuration with Hydrocarbon Fuel”, International Workshop on Combustion and Propulsion, Pozzuoli. June 2002.

2. R. Monti, R. Savino, G. Pezzella, et al., “Aerothermodynamics Study of an Advanced Thermal Protection System”, 4

th European Workshop on hot Structure and Thermal Protection System for Space Vehicles, ESA.

Palermo, Nov 2002. ESA SP-521 April 2003.

3. G. Pezzella, R. Monti, “Analisi di un Veicolo Rientrante a Bordi d'Attacco Aguzzi”, XVII° Congresso dell'Associazione Italiana di Aeronautica ed Astronautica (AIDAA). Roma, September 2003.

4. R. Monti, G. Pezzella, “Low Risk Re-Entry Vehicle”, 12th AIAA International Space Planes and Hypersonic

Systems and Technologies Conference. Norfolk, Virginia (USA), Dec 15-19, 2003. AIAA-2003-7019.

5. R. Monti, G. Pezzella, “Design Criteria for Low Risk Re-Entry Vehicles”, Fifth European Symposium on Aerothermodynamics for Space Vehicles. 8-11 Nov 2004 Cologne, Germany.

6. A. Schettino, G. Pezzella, et al., “Mission Trade-off Analysis of the Italian USV Re-Entry Flying Test Bed”, 14th

AIAA/AHI International Space Planes and Hypersonic Systems and Technologies Conference. 6-9 Nov. 2006, Canberra (Australia), paper AIAA-2006-8017.

7. A. Schettino, G. Pezzella, et al., “Aero-thermal Trade-off Analysis of the Italian USV Re-Entry Flying Test Bed”, 14

th AIAA/AHI International Space Planes and Hypersonic Systems and Technologies Conference. 6-9 Nov.

2006, Canberra (Australia), paper AIAA-2006-8114.

8. A. Viviani, G. Pezzella, D. Cinquegrana, “Aerothermodynamic Analysis of an Apollo-like Reentry Vehicle”, 14th

AIAA/AHI International Space Planes and Hypersonic Systems and Technologies Conference. 6-9 Nov. 2006, Canberra (Australia), paper AIAA-2006-8082.

9. A. Viviani, G. Pezzella, “Analisi Aerotermodinamica di un Veicolo di Rientro Tipo Capsula Apollo”. Giornate Scientifiche di Ateneo 2007. Seconda Università Di Napoli. IN-I-026.

10. A. Viviani, G. Pezzella, “Catalytic Effects on Non-Equilibrium Aerothermodynamic of a Reentry Vehicle”, 45th

AIAA Aerospace Science Meeting and Exhibit, 8-11 Jan. 2007, Reno, NE (USA); paper AIAA-2007-1211.

11. A. Viviani, G. Pezzella, “Influence of Surface Catalyticity on Reentry Aerothermodynamics and Heat Shield”, 39th

AIAA Thermophysics Conference, 25-28 Jun. 2007, Miami, FL (USA); paper AIAA-2007-4047.

12. E. Bucchignani, G. Pezzella, “Numerical investigations of classical hypersonic problems; comparison with experimental data”, 7

th IMACS/ISGG Meeting on Applied Scientific Computing and Tools Grid Generation,

Approximation, and Visualization (MASCOT07). Sept. 13-14, 2007, Roma. (Invited paper).

13. G. Pezzella, F. Battista, et al., “Hypersonic Aerothermal Environment Preliminary Definition of the CIRA FTB-X Reentry Vehicle”, WEHSFF 2007 West-East High Speed Flow Field Conference 2007, Moscow, Nov 19-22, 2007.

14. A. Viviani, G. Pezzella, S. Borrelli, “Effect of Finite Rate Chemical Models on the Aerothermodynamics of Reentry Capsules”, 15

th AIAA/AHI International Space Planes and Hypersonic Systems and Technologies

Conference. Apr. 28-1, 2008. Dayton, Ohio (USA), paper AIAA-2008-2668.

15. G. Pezzella, M. Marini, and P. Roncioni, J. Kauffmann, C. Tomatis, “Aerodynamic and Aerothermodynamic Evaluation of the VTO Hopper Concept in the Frame of ESA Future Launchers Preparatory Program”, 15

th AIAA

International Space Planes and Hypersonic Systems and Technologies Conference. Apr. 28-1, 2008. Dayton, Ohio (USA), paper AIAA-2008-2639.

16. A. Viviani, G. Pezzella, C. Golia, “Effects of Surface Catalyticity on Computed Heat Transfer over a Reentry Vehicle”, Proceedings of CHT-08 ICHMT International Symposium on Advances in Computational Heat



Transfer. May 11-16, 2008, Marrakech, Morocco. Paper CHT-08-330.

17. E. Bucchignani, G. Pezzella, “A Spline Based Algorithm for the Analysis of the Flow in Scirocco Plasma Wind Tunnel Nozzle”, 8

th IMACS/ISGG Meeting on Applied Scientific Computing and Tools Grid Generation,

Approximation, and Visualization (MASCOT08). Oct. 23-25, 2008, Roma. (Invited paper).

18. A. Viviani, G. Pezzella, C. Golia, “Analysis of Thermochemical Modeling and Surface Catalyticity in Space Vehicles Reentry”, Proceedings of 26

th International Congress of the Aeronautical Sciences – ICAS 2008. Sept

14-19, 2008, Anchorage, ALASKA. Paper ICAS 2008-3.6.2.

19. E. Bucchignani, G. Pezzella, A. Matrone, “Numerical Simulation of Liquid-Structure Interaction Problems in a Tank for Aerospace Applications”, 6

th European Symposium on Aerothermodynamics for Space Vehicles, ESA

sponsored Conference. 3-5 November 2008, Versailles. France.

20. G. Pezzella, E. Bucchignani, M. Marini, G. Ferraris, C. Chiarelli, “Computational Aeroheating Analyses of a Capsule in Martian Atmosphere”, 6

th European Workshop on Thermal Protection Systems and Hot Structures,

March 31st – April 3rd, 2009 University Stuttgart, Germany

21. G. Pezzella, J. Kauffmann, A. Dapra, C. Tomatis, “An Italian Contribution to the Next Generation Launcher in the Framework of ESA Future Launchers Preparatory Programme”, XX AIDAA Congress, Milano, Italy, June 29-July 3, 2009.

22. A. Viviani, L. Savino, G. Pezzella, “Dependence and Sensitivity on the Aerothermochemical Model of Atmospheric Reentry Trajectories”, 3

rd EUCASS European Conference for Aero-Space Sciences. 6-9 July

2009, Versailles – Paris (France). EUCASS2009-182.

23. G. Pezzella, E. Filippone, M. Serpico, “Re-entry Aerodynamics and Aerothermodynamics Analyses of the Flying Test Bed USV-X in the Framework of a High Lift Return”, 16

th AIAA/DLR/DGLR International Space Planes and

Hypersonic Systems and Technologies Conference. Bremen, Germany, Oct. 19-22, 2009. AIAA-2009-7425.

24. G. Pezzella, M. Marini, J. Kauffmann, A. Dapra, C. Tomatis, “Appraisal of Aerodynamics and Aerothermodynamics of RFS and LFBB (LOx/CH4) ESA Future Launchers Preparatory Program Concepts”, 16

th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference.

Bremen, Germany, Oct. 19-22, 2009. AIAA-2009-7340.

25. G. Pezzella, R. Votta, “Finite Rate Chemistry Effects on the High Altitude Aerodynamics of an Apollo-Shaped Reentry Capsule”, 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. Bremen, Germany, Oct. 19-22, 2009. AIAA-2009-7306.

26. A. Viviani, G. Pezzella, “Aerodynamic Analysis of a Capsule Vehicle for a Manned Exploration Mission to Mars”, 16

th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference.

Bremen, Germany, Oct. 19-22, 2009. AIAA-2009-7386.

27. A. Viviani, G. Pezzella, C. Golia, “Effects of Thermochemical Modeling and Surface Catalyticity on an Earth Reentry Vehicle”, CEAS 2009 European Air and Space Conference. 26-29 October 2009. Manchester, UK.

28. A. Viviani, G. Pezzella, “Computational Heat Transfer Analyses for a Winged Reentry Vehicle”, 4th International

Conference on Thermal Engineering: Theory and Application. Abu Dhabi, United Arab Emirates, January 12-14, 2009. Paper # 293. ISBN-978-9948-03-941-9.

29. A. Viviani, G. Pezzella, C. Golia, “Aerodynamic and Thermal Design of a Space Vehicle Entering the Mars Atmosphere”, Proceedings of fifth International Conference on Thermal Engineering: Theory and Applications. ICTEA 2010. May 10-14, 2010, Marrakesh, Morocco.

30. A. Viviani, G. Pezzella, C. Golia, “Aerothermodynamic Analysis of a Space Vehicle for Manned Exploration Missions to Mars”, Proceedings of 27

th International Congress of the Aeronautical Sciences. ICAS 2010. Nice,

France 19-24 September, 2010.

31. G. Pezzella, Marini M., Rufolo G., “Aerodynamic Characterization of the ESA Intermediate Experimental Vehicle”, 17

th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. San

Francisco, California. Apr. 11-14, 2011. AIAA-2011-2232.



32. A. Viviani, Pezzella G., “Aerothermochemical Flowfield around Space Vehicles for Manned Missions to Mars”. 17

th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. San Francisco,

California. Apr. 11-14, 2011. AIAA-2011-2272.

33. Pezzella G., Gardi R., Guidotti G., Richiello C., “Aerodynamic and Aerothermodynamic Trade-off Analysis of the Italian USV2 Flying Test Bed in the Framework of an Hypersonic Flight Test”. 3

rd International ARA Days. 2-4

May 2011. Arcachon. France. AA-1-2011-54.

34. Gardi R., Pezzella G., Del Vecchio A., Marino G., Russo G., “Sounding Hypersonic Atmospheric Reentry Capsule Shark. Design Realization Flight and Data Interpretation”. 3rd International ARA Days. 2-4 May 2011. Arcachon. France. AA-1-2011-36.

35. G. Guidotti, G. Pezzella, C. Richiello, G. Russo, S. C. Tirtey, R.R. Boyce, “Preliminary Analysis of the USV_2 Hypersonic Flight Test”. 7

th European Symposium on Aerothermodynamics for Space Vehicles. European

Space Agency (ESA). 9 - 12 May 2011. Site Oud Sint-Jan, Brugge. Belgium.

36. G. Pezzella, C. Richiello, G. Russo, “Assessment of the Aerodynamic and Aerothermodynamic Performance of the USV-3 High-Lift Reentry Vehicle”. 7

th European Symposium on Aerothermodynamics for Space Vehicles.

European Space Agency (ESA). 9 - 12 May 2011. Site Oud Sint-Jan, Brugge. Belgium.

37. A. Viviani, G. Pezzella, “Non-Equilibrium Computational Flowfield Analysis for Mars Entry Manned Vehicles”. 4th

European Conference for Aerospace Sciences (EUCASS). Saint Petersburg, Russia. July 4, 2011 – July 8, 2011 ID522.

38. A. Viviani, L. Iuspa, G. Lanzillo, G. Pezzella, “Preliminary Design of Minimum Weight Configurations for a Re-Entry Vehicle”. The International Conference of the European Aerospace Societies CEAS 2011. Venice, Italy. October 24

th – 28

th, 2001.

39. G. Pezzella, P. Catalano, G. Mingione, “Aerodynamics and Aerothermodynamics Appraisal of the CIRA High-Lift Re-entry Vehicle”, 3

rd Sino-Italian Conference on Space Aerothermodynamics and Hot Structures. Shanghai .

China. November 21-23, 2011.

40. A. Viviani, G. Pezzella, C. Golia, “Aerothermodynamic Field Past a Re-entry Capsule for Sample Return Missions”, 28

th International Congress of the Aeronautical Sciences. ICAS-2012. 23 - 28 September, 2012,

Brisbane, Australia.

41. G. Pezzella, P. Catalano, A. Bourgoing, “Computational Flowfield Analysis of a Sample Return Capsule”, 18th

AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference. 24-28 September, 2012, Tours. France. AIAA-2012-5818.

42. A. Viviani, G. Pezzella, “Overview of Design Approach for a Sample Return Capsule”, 18th AIAA/3AF

International Space Planes and Hypersonic Systems and Technologies Conference. 24-28 September, 2012, Tours. France. AIAA-2012-5858.

43. A. Viviani, G. Pezzella, “Aerodynamic Performance Analysis of an Unmanned Re-Entry Vehicle from Hypersonic Down to Subsonic Regime”, 63

rd International Astronautical Congress. IAC-2012. 1-5 Oct. 2012.

Naples, Italy. IAC-12-D2.3.4

44. D. Cinquegrana, G. Pezzella, P. Catalano, M. De Stefano Fumo, F. Petrosino, G. Mingione, “A POD-Based Reduced Order Model for the Simulation of Scirocco PWT Nozzles”, 63

rd International Astronautical Congress.

IAC-2012. 1-5 Oct. 2012. Naples, Italy. IAC-12-D1.3.6.

45. G. Pezzella, G. Rufolo, G. Marino, “Aerodynamic Performance Analysis of the IXV Vehicle”, 63rd International

Astronautical Congress. IAC-2012. 1-5 Oct, 2012. Naples, Italy. IAC-12-D2.6.3.p1

46. G. Pezzella, P. Catalano, M. De Stefano Fumo, D. Cinquegrana, F. Petrosino, E. Trifoni, A. Bourgoing, “Aerodynamics and Aerothermodynamics Analyses of a Earth-Re-Entry Capsule for Sample Return Mission in the Framework of RASTAS SPEAR Project”, 63

rd International Astronautical Congress. IAC-2012. 1-5 Oct.

2012. Naples, Italy. IAC-12-A3.5.14.p1

47. F. Petrosino, M. De Stefano Fumo, G. Pezzella, P. Catalano, D. Cinquegrana, G. Mingione, “Aerodynamic Performances of USV3 CIRA Re-Entry Vehicle”, 63

rd International Astronautical Congress. IAC-2012. 1-5 Oct,



2012. Naples, Italy. IAC-12-D2.3.7.

48. G. Pezzella, E. Trifoni, “Aerothermodynamic Design of an Ablative Heat Shield for a Sample Return Vehicle”, 4th

Sino-Italian Conference on Space Aerothermodynamics and Hot Structures. November 28-30, 2012. Capua. Italy.

49. F. Petrosino, M. De Stefano Fumo, G. Pezzella, “Aerodynamic Analysis of Unmanned Re-Entry Vehicle Concepts from M=0.3 to 25”, 4

th Sino-Italian Conference on Space Aerothermodynamics and Hot Structures.

November 28-30, 2012. Capua. Italy.

50. F. Petrosino, G. Andreutti, G. Pezzella, P. Catalano, M. De Stefano Fumo, “Aerodynamic Analysis of Unmanned Re-Entry Vehicle Concepts from M=0.3 to 25”, 4

th International Ara Days. May 27-29, 2013 Arcachon. France.

51. F., Petrosino, M., De Stefano Fumo, G. Pezzella, “Aerodynamic Analysis of Unmanned Re-Entry Vehicle Concepts from M=0.3 to 25”, 29th International Symposium on Space Technology and Science. Nagoya, Japan, 2 ‐ 9 June 2013.

52. A. Viviani, G. Pezzella, “Analysis of Flowfield Past a Sample Return Capsule with Heatshield Ablation”, 44th

AIAA Thermophysics Conference. 24 - 27 June 2013. San Diego, California. doi: 10.2514/6.2013-2775.

53. F. Petrosino, M. De Stefano Fumo, G. Pezzella, “Evolution of Aerodynamic Shape for a Concept of Autonomous Re-Entry Vehicle”, 31

st AIAA Applied Aerodynamics Conference. 24 - 27 June 2013. San Diego, California. doi:

10.2514/6.2013-2664.

54. A. Viviani, G. Pezzella, “Computational analysis of the flowfield past a returning capsule at super-orbital speed”, 5

th European Conference for Aeronautics and Space Sciences (EUCASS2013). Munich, Germany - July 1-5,

2013. A252.

55. A. Viviani, G. Pezzella, “Aerodynamic Performance Analysis of Three Different Vehicle Concepts at Hypersonic Speed”, XXII Conference of Italian Association of Aeronautics and Astronautics (AIDAA 2013). Naples, Italy - September 9-12, 2013. A-74.

56. G. Buonomo, M. Musto, N. Bianco, G. Rotondo, G. Pezzella, G. Mingione, “Aerothermal Analysis of an Aircraft Nacelle in the Framework of a Fully Coupled Approach”, XXII Conference of Italian Association of Aeronautics and Astronautics (AIDAA 2013). Naples, Italy - September 9-12, 2013. A-82.

57. D. Cinquegrana, G. Pezzella, P. Catalano, “Aerodynamic and Aerothermodynamic of the USV3 Re-entry Vehicle”, XXII Conference of Italian Association of Aeronautics and Astronautics (AIDAA 2013). Naples, Italy - September 9-12, 2013. A-78.

58. A. Carozza, G. Mingione, G. Pezzella, “Computational Flow Field Analyses on Aeronautical Oil Cooling Systems”, XXII Conference of Italian Association of Aeronautics and Astronautics (AIDAA 2013). Naples, Italy - September 9-12, 2013. A-112.

59. G. Buonomo, M. Musto, N. Bianco, G. Rotondo, G. Pezzella, G. Mingione, “Sensitivity Analysis for the Numerical Simulation of an Engine Air Cooling System”, XXII Conference of Italian Association of Aeronautics and Astronautics (AIDAA 2013). Naples, Italy - September 9-12, 2013. A-141.

60. D. Cinquegrana, G. Pezzella, P. Catalano, “A reduced Order Model for a Rapid Evaluation of Scirocco PWT Nozzles Flowfield”, XXII Conference of Italian Association of Aeronautics and Astronautics (AIDAA 2013). Naples, Italy - September 9-12, 2013. A-153.

61. F. Petrosino, D. Cinquegrana, G. Andreutti, F. Capizzano, P. Catalano, G. Pezzella, M. De Stefano Fumo, “Aerodynamic Analysis of the USV3 Vehicle from Hypersonic to Landing Flight Conditions”, 64

rd International

Astronautical Congress. IAC-2013. 23-27 Sept, 2013. Beijing, China. IAC-13-D2.3.

62. D. Cinquegrana, R. Gardi, V. De Simone, F. Petrosino, P. Catalano, G. Pezzella, M. De Stefano Fumo, “Aerothermodynamic and TPS Design Analysis of the USV3 Re-Entry Vehicle”, 64

rd International Astronautical

Congress. IAC-2013. 23-27 Sept, 2013. Beijing, China. IAC-13-D2.3.1.19286.

63. G. Pezzella, M. Marini, M. Cicala, A. Vitale, T. Langener , J. Steelant, “Aerodynamic Characterization of



HEXAFLY Scramjet Propelled Hypersonic Vehicle”. 32nd

AIAA Aviation (Applied Aerodynamics Conference). 16-20 June 2014, Atlanta, GA. AIAA 2014-2844.

64. D. Cinquegrana, F. Petrosino, G. Pezzella, F. Capizzano, G. Andreutti, P. Catalano, M. De Stefano Fumo, “USV3 Aerodynamics Assessment: a Step Forward in the Ongoing Design Phase”. 45

th AIAA Plasmadynamics and

Lasers Conference, 2014, 10.2514/6.2014-2379. AIAA 2014-2379

65. A. Viviani, G. Pezzella, “Hypersonic Aerodynamic Appraisal of Winged Blunt, Rather Sharp and Spatuled Body Re-entry Vehicles”, 29

th Congress of the International Council of the Aeronautical Sciences. September 7–12,

2014. St. Petersburg, Russia. Paper (4.7.5).

66. M. De Stefano Fumo, A. Pugliese, G. Pezzella, G. Guidotti, “Small Autonomous Winged Aeroshape Trade-off through Mission and System Guidelines”. 65

th International Astronautical Congress. Toronto, Canada. 29

th Sept-

3rd Oct. 2014. IAC-14-D2.6.6.

67. D. Cinquegrana, G. Pezzella, P. Catalano, M. De Stefano Fumo, “The CIRA Effort Toward a Fast Aerothermal Design Environment Tool”. 65

th International Astronautical Congress. Toronto, Canada. 29

th Sept- 3

rd Oct. 2014.

IAC-14-D1.6.8.

68. A. Viviani, G. Pezzella, “Aerodynamic Analysis of an Unmanned Aerial Vehicle at Hypersonic Speed”, 65th

International Astronautical Congress. Toronto, Canada. 29th Sept- 3

rd Oct. 2014. IAC-14, D2,3.10.

69. G. Pezzella, S. van Brummen, J. Steelant, “Assessment of Hypersonic Aerodynamic Performance of the EFTV-ESM Configuration in the Framework of the Hexafly-Int Research Project”, 8

th European Symposium on

Aerothermodynamics for Space Vehicles. 2-6 March 2015. Lisbon. Portugal. European Space Agency.

70. G. Pezzella, V. Carandente, R. Scigliano, M. Marini, J. Steelant, “Aerothermal Environment Methodology of the Hexafly-Int Experimental Flight Test Vehicle (EFTV)”, 8

th European Symposium on Aerothermodynamics for

Space Vehicles. 2-6 March 2015. Lisbon. Portugal. European Space Agency.

71. D. Cinquegrana, F. Capizzano, F. Petrosino, P. Catalano, G. Pezzella, M. De Stefano Fumo, “A Fast Pod-Based Aerothermal Design Environment Tool”, 8

th European Symposium on Aerothermodynamics for Space Vehicles.

2-6 March 2015. Lisbon. Portugal. European Space Agency.

72. P. Catalano, G. Andreutti, F. Capizzano, D. Cinquegrana, M. De Stefano Fumo, G. Pezzella, P. di Patria, “Assessment of Aero-Thermodynamic Characteristics of the USV3 Vehicle”, 8

th European Symposium on

Aerothermodynamics for Space Vehicles. 2-6 March 2015. Lisbon. Portugal. European Space Agency.

73. A. Viviani, G. Pezzella, “Computational Flowfield Analysis of a Next Generation Launcher”. 6th European

Conference for Aeronautics and Space Sciences (Eucass). 29 June- 3 July. 2015 Krakow. Poland.

74. G. Pezzella, D. de Rosa, R. S. Donelli and P. Catalano, “Numerical Rebuilding of High and Low Enthalpy Hypersonic Flow Test Over a Double Wedge Model”. 6

th European Conference for Aeronautics and Space

Sciences (Eucass). 29 June- 3 July. 2015 Krakow. Poland.

75. V. Carandente, R. Scigliano, G. Pezzella, M. Marini, and J. Steelant, “Finite Element Thermal Design of the Hexafly-INT Experimental Flight Test Vehicle”. 6

th European Conference for Aeronautics and Space Sciences

(Eucass). 29 June- 3 July. 2015 Krakow. Poland.

76. F. Piscitelli, L. Cutrone, G. Pezzella, P. Roncioni, M. Marini, “SPREAD: a simplified tool for the nose of an airbreathing hypersonic vehicle”. 6

th European Conference for Aeronautics and Space Sciences (Eucass). 29

June- 3 July. 2015 Krakow. Poland.

77. G. Pezzella, M. Marini, B. Reimann, and J. Steelant, “Aerodynamic Design Analysis of the HEXAFLY-INT Hypersonic Glider”. 20

th AIAA Hypersonics. Strathclyde University Technology & Innovation Center. 6-9 July

2015 Glasgow. Scotland. AIAA-2015-3644. doi: 10.2514/6.2015-3644.

78. G. Pezzella, D. de Rosa, and R. S. Donelli, “Computational Analysis of Shock Wave Boundary Layer Interactions in Non-equilibrium Hypersonic Flow”, 20

th AIAA Hypersonics. Strathclyde University Technology &

Innovation Center. 6-9 July 2015 Glasgow. Scotland. AIAA-2015-3578. doi: 10.2514/6.2015-3644.



79. A. Viviani, G. Pezzella, “Numerical Analysis of the Flowfield Past a Next Generation Launcher”. 20th AIAA

Hypersonics. Strathclyde University Technology & Innovation Center. 6-9 July 2015 Glasgow. Scotland. AIAA-2015-3535. doi: 10.2514/6.2015-3644.

80. N. Favaloro, G. Pezzella, V. Carandente, R. Scigliano, M. Cicala, G. Morani, J. Steelant, “Design Analysis of the High-Speed Experimental Flight Test Vehicle HEXAFLY-International”. 20

th AIAA Hypersonics. Strathclyde

University Technology & Innovation Center. 6-9 July 2015 Glasgow. Scotland. AIAA-2015-3607. doi: 10.2514/6.2015-3644.

81. J. Steelant, T. Langener, F. Di Matteo, K. Hannemann, J. Riehmer, M. Kuhn, C. Ditter, W. Jung, M. Marini, G. Pezzella, M. Cicala, L. Serre, “Conceptual Design of the High-Speed Propelled Experimental Flight Test Vehicle HEXAFLY”. 20

th AIAA Hypersonics. Strathclyde University Technology & Innovation Center. 6-9 July 2015

Glasgow. Scotland. AIAA-2015-3539. doi: 10.2514/6.2015-3644.

82. A. Carozza, G. Mingione, G. Serino, G. Pezzella, “Thermal investigation of a nacelle internal and external fields in pusher configuration”. XXIII Conference of Italian Association of Aeronautics and Astronautics (AIDAA 2015). Turin, Italy - November 16-19, 2015.

83. D. de Rosa, G. Pezzella, R. S. Donelli, “Numerical assessment of flap effectiveness for winged re-entry vehicles”. XXIII Conference of Italian Association of Aeronautics and Astronautics (AIDAA 2015). Turin, Italy - November 16-19, 2015.

84. P. Roncioni, G. Pezzella, M. Marini, J. Steelant, “Numerical simulations of the HEXAFLY-INT experimental vehicle”. XXIII Conference of Italian Association of Aeronautics and Astronautics (AIDAA 2015). Turin, Italy - November 16-19, 2015.

85. R. Scigliano, G. Pezzella, M. Marini, S. Di Benedetto, J. Steelant, “Aerothermal Design of the Hexafly-int Glider”. SPACE Conferences and Exposition, 13-16 September 2016, Long Beach, California AIAA 2016-5627. DOI: 10.2514/6.2016-5627.

86. J. Steelant, V. Villace, M. Marini, G. Pezzella, B. Reimann, S.L. Chernyshev, A.A. Gubanov, V.A. Talyzin, N.V. Voevodenko, N.V. Kukshinov, A.N. Prokhorov, A.J. Neely, C. Kennell, D. Verstraete, D. Buttsworth, “Numerical and Experimental Research on Aerodynamics of High Speed Passenger Vehicle within the Hexafly-Int Project”. 30

th Congress of International Council of the Aeronautical Sciences. ICAS 2016. DDC Daejeon Korea.

September 25-30, 2016.

87. A. Viviani, G. Pezzella, E. D’Amato, “Aerodynamic Analysis with Separation Dynamics of a Launcher at Staging Conditions”. 30

th Congress of International Council of the Aeronautical Sciences. ICAS 2016. DDC Daejeon

Korea. September 25-30, 2016.

88. M. Marini, G. Pezzella, A. Schettino, S. Di Benedetto, V. Fernandez Villace, J. Steelant, A. Gubanov, N. Voevodenko, B. Reimann, and C. Walton. "Numerical and Experimental Aerodynamic Characterization of the HEXAFLY-INT Hypersonic Glider", 21

st AIAA International Space Planes and Hypersonics Technologies

Conference, International Space Planes and Hypersonic Systems and Technologies Conferences, (AIAA 2017-2316). http://dx.doi.org/10.2514/6.2017-2316

89. R. Votta, E. Trifoni, G. Pezzella, M. Di Clemente, A. Schettino, V. Mareschi, P. Venditto, A. Ferri, J. Alves, L. Ferracina, “Numerical Investigation of RCS Jet Interaction and Plume Impingement for Mars Precision Landing”. 8

th AIAA Theoretical Fluid Mechanics Conference. AIAA AVIATION Forum. Denver. Colorado. (AIAA

2017-3350). https://doi.org/10.2514/6.2017-3350

90. R. Gardi, A. Fedele, G. Pezzella, P. Vernillo, S. Mungiguerra, P. Dell’Aversana, L. Gramiccia, K. J. Henriksson, J. Smith, “MINI-IRENE: Design of a Capsule with Deployable Heat Shield for a Sounding Rocket Flight Experiment”. 23

rd ESA Symposium on European Rocket and Balloon Programmes and Related Research. 11 –

15 June 2017. Visby – Sweden. Paper A-32.

91. R. Gardi, A. Fedele, G. Pezzella, P. Vernillo, R. Savino, S. Mungiguerra, P. Dell' Aversana, L. Gramiccia, K. Henriksson, J. Smith, J. Longo, “MINI-IRENE: Design of Deployable Heat Shield Capsule for a Sounding Rocket Flight Experiment”. 68

th International Astronautical Congress, Adelaide, Australia. IAC-17-D2.6.2.

92. R. Gardi, P. Vernillo, A. Fedele, G. Pezzella, R. Savino, P. Dell’Aversana, L. Gramiccia, G. D’aniello, R. Aurigemma, N. Cimminiello, F. Punzo, G. Florin, R. Molina. “MINI IRENE - Deployable Heat Shield for



Suborbital Flight Test”. XXIV International Conference of Italian Association of Aeronautics and Astronautics AIDAA. 18-22 September 2017, Palermo – Enna, Italy.

93. R. Gardi, G. Pezzella, S. Franchitti, R. Borrelli, C. Pirozzi, V. Quaranta, B. Tiseo, G. Bruno, “Additive Layer Manufacturing For Entry Capsules” 68

th International Astronautical Congress, Adelaide, Australia. IAC-17-

C2.9.10.

94. R. Scigliano, G. Pezzella, S. Di Benedetto, M. Marini, J. Steelant, “Hexafly-Int Experimental Flight Test Vehicle (EFTV) Aero-Thermal Design”. Proceedings of the ASME 2017 International Mechanical Engineering Congress & Exposition IMECE 2017. November 3-9, 2017, Tampa, Florida, USA. ASME 2017 International Mechanical Engineering Congress and Exposition Volume 1: Advances in Aerospace Technology Tampa, Florida, USA, November 3–9, 2017.Conference Sponsors: ASME ISBN: 978-0-7918-5834-9. Paper No. IMECE2017-70392, pp. V001T03A022; 14 pages doi:10.1115/IMECE2017-70392.

95. A. Viviani, G. Pezzella, “Launcher Aerodynamic Analysis With Plume Effects” 31st Congress f the International

Council of Aeronautical Sciences. Belo Horizonte. Brazil . September 9-14 2018.

96. T. Bykerk, D. Verstraete, G. Pezzella, A. Viviani. “High and Low Speed Analysis of a Re-usable Unmanned Re-entry Vehicle”. HISST. International Conference on High-Speed Vehicle Science and Technology. Moscow. Russia. November 25-29, 2018. hisst-2018_1620897.

97. A. Schettino, G. Pezzella, M.Marini, S.Di Benedetto, V.F. Villace, J. Steelant, A.Gubanov, N. Voevodenko “Aerodynamic and Aerothermodynamic Database of the HEXAFLYINT Hypersonic Glider”. HISST. International Conference on High-Speed Vehicle Science and Technology. Moscow. Russia. November 25-29, 2018. hisst-2018_2940957.

98. S. Di Benedetto, M. P. Di Donato, A. Rispoli, G. Pezzella, R. Scigliano, F. Nebula, D. Cristillo, L. Vecchione; S. Cardone; J. Steelant, V. Villace. “Multidisciplinary Design and Flight Test of the HEXAFLY-INT Experimental Flight Vehicle”. HISST. International Conference on High-Speed Vehicle Science and Technology. Moscow. Russia. November 25-29, 2018. hisst-2018_42601154

TUTORSHIP Tesi di Laurea

1. Influenza della Modellistica Termochimica nella Traiettoria di Rientro in Atmosfera Terrestre. Candidato Davide Cinquegrana. AA 2004/2005. Seconda Università di Napoli. Facoltà di Ingegneria. Relatore Prof. Antonio Viviani.

2. Ottimizzazione di configurazione e traiettoria di un veicolo lifting body per rientro spaziale. Candidato Giovanni Lanzillo. AA 2009/2010. Seconda Università di Napoli. Facoltà di Ingegneria. Relatore Prof. Antonio Viviani.

3. Non-Equilibrium Computational Analysis around a Super-Orbital Re-Entry Capsule with Ablation. Candidato Domenico Cristillo. AA 2010/2011. Seconda Università di Napoli. Facoltà di Ingegneria. Relatore Prof. Antonio Viviani.

4. Non-Equilibrium Computational Analysis of the Flowfield past a Super-Orbital Re-Entry Capsule with Plasma Radiation. Candidato Roberto Gallo. AA 2010/2011. Seconda Università di Napoli. Facoltà di Ingegneria. Relatore Prof. Antonio Viviani.

5. Computational Thermo-Fluid Dynamics Analysis of an Aircraft’s Turboprop Oil Cooler System and Comparison with Experimental Data. Candidato Lorenzo Barbato. AA 2011/2012. Università di Napoli “Federico II”. Facoltà di Ingegneria. matr. 354/197. Relatore Prof. Nicola Bianco.

6. Aerothermal Analysis of an Aircraft Nacelle in the Framework of a Fully Coupled Approach. Candidato Gennaro Buonomo. AA 2012/2013. Università di Napoli “Federico II”. Facoltà di Ingegneria. matr. 65/122. Relatore Prof. Nicola Bianco.

7. High Speed Centrifugal Compressor for Aircraft Engines. Candidato Salvatore Vivenzio. AA 2012/2013. Università di Napoli “Federico II”. Facoltà di Ingegneria. matr. N35/000724. Relatore Prof. Gennaro Cardone.

8. Aerodynamic Design of a Hypersonic Aircraft Powered with Scramjet Engine. Candidata Eliana Russo. AA 2012/2013. Seconda Università di Napoli. Scuola Politecnica e delle Scienza di Base. Corso di Laurea in Ingegneria Aerospaziale. matr. A15/000012. Relatore Prof. Antonio Viviani.



9. A Thermo-Fluid Dynamic Analysis of an Oil Cooling System for a Turboprop Engine in Ground and Cruise Conditions. Candidato Flavio Toscano. AA 2013/2014. Università di Napoli. Scuola Politecnica e delle Scienza di Base. Corso di Laurea in Ingegneria Meccanica. matr. M65000213. Relatori Proff. Marilena Musto, Nicola Bianco, Giuseppe Rotondo.

10. Coupled Flowfield Analysis and Separation Dynamics of Experimental Flight Test Vehicle (EFTV) and Experimental Support Module (ESM). Candidata Cinzia Rainone. AA 2014/2015. Seconda Università di Napoli. Scuola Politecnica e delle Scienza di Base. Corso di Laurea in Ingegneria Aerospaziale. matr. A15/000050. Relatore Prof. Antonio Viviani.

11. Appraisal of the Aerodynamic Performance of a Flying Test Bed Vehicle in the Framework of the Build-up Approach. Candidato Luigi Aimone. AA 2014/2015. Università degli Studi di Napoli “Federico II”. Scuola Politecnica e delle Scienza di Base. Dipartimento di Ingegneria Industriale. Corso di Laurea in Ingegneria Aerospaziale. matr. M53/195. Relatore Prof. Carlo de Nicola.

12. Analysis of Reaction Control System Jet-Interaction for a Mars Entry Capsule. Candidato Michele Ventriglia. M53/506. AA 2016/2017. Università degli Studi di Napoli “Federico II”. Scuola Politecnica e delle Scienza di Base. Dipartimento di Ingegneria Industriale. Corso di Laurea Magistrale in Ingegneria Aerospaziale. Relatore Prof. Carlo de Nicola.

13. An optimization framework for hypersonic vehicle design. Candidato Simone Di Giorgio. ID number 1412208. AA 2016/2017. Università degli Studi di Roma “Sapienza”. Facoltà di Ingegneria Civile e Industriale. Corso di Laurea Magistrale in Ingegneria Aeronautica. Relatore Prof. Sergio Pirozzoli.

TUTORSHIP Tesi di Dottorato

1. Influenza della Modellistica Termochimica sulla Traiettoria di Rientro. Candidato Luigi Savino. Dottorato di ricerca in scienze e tecnologie aerospaziali. XXI° Ciclo. Seconda Università di Napoli. Facoltà di Ingegneria.

Coinvolgimento in Progetti di Ricerca

Programmi Italiani

1. PRORA (PROGRAMMA NAZIONALE RICERCA AEROSPAZIALE). Aerodynamic analysis and aerodynamic database development of several flying test bed concepts (USV, Unmanned Space Vehicle) USV1, USV2, USV3. Phase-A design.

2. FLECS (MODULO GONFIABILE ESPANDIBILE PER ABITABILITA’ UMANA NELLO SPAZIO). Italian Space Agency (ASI). Aerothermodynamic analysis of loading conditions for a Mars Entry Mission.

3. HYTAM (HYPERSONIC TACTIC MISSILE). SEGREDIFESA. Aeroshape design of a hypersonic airbreathing configuration. Aerodynamic and aerothermodynamic analysis.

4. SHARK (SOUNDING HYPERSONIC ATMOSPHERIC REENTRY CAPSULE). Aerodynamic and aerothermodynamic design analysis of a flying test bed capsule for UHTC in-flight experimentation. Post flight analysis. Data reconstruction.

5. VECEP (VEGA CONSOLIDATION AND EVOLUTION PREPARATION). AVIO. Aerodynamic and aerothermodynamic analysis of VEGA-C3 configuration. Effects of surface protrusions and aerodatabase of several stage configurations (intact and/or fragmented one) of the VEGA C3 launcher.

6. VEGAL. AVIO. Aerodynamic and aerothermodynamic analysis of MINI VEGA configuration.

Programmi Internazionali

1. FLPP (FUTURE LAUNCHER PREPARATORY PROGRAMME). European Space Agency. Aerodynamic performance analysis and Aerodynamic database development of four launchers concept. Phase-A design.

2. EXPERT (EUROPEAN EXPERIMENTAL REENTRY TESTBED), European Space Agency. Aerodynamic performance analysis and aerodynamic database development.



3. IXV (INTERMEDIATE EXPERIMENTAL VEHICLE), European Space Agency. Aerodynamic performance analysis and Aerodynamic database development. Phase-C1, Phase-D design, ASI-Technical Assistance.

4. SCRAMSPACE (SCRAMJET-BASED ACCESS-TO-SPACE SYSTEMS). UQ's Centre for Hypersonics and the Defense, Science and Technology Organization's (DSTO) Applied Hypersonics Branch in Brisbane. Aerothermodynamic design of a flight passenger experiment.

5. RASTAS SPEAR (RADIATION-SHAPES-THERMAL PROTECTION INVESTIGATIONS FOR HIGH SPEED EARTH RE-ENTRY). Seventh Framework Programme: Project number FP7/SPACE/241992. Aerodynamic and Aerothermodynamic design of a heat shield for a sample return capsule with TPS ablation and plasma radiation.

6. LAPCAT II (LONG-TERM ADVANCED PROPULSION CONCEPTS AND TECHNOLOGIES), Seventh Framework Programme. Aerodynamic and Aerothermodynamic design of an airbreathing configuration.

7. HEXAFLY (HIGH-SPEED EXPERIMENTAL FLY VEHICLES). Seventh Framework Programme. Aerodynamic and Aerothermodynamic design of an airbreathing configuration.

8. CFD simulation activities of NATO Science and Technology Organization (STO) Applied Vehicle Technology (AVT) Panel. Task Group 205 “Assessment of Predictive Capabilities for Aerothermodynamic Heating of Hypersonic Systems". (2011-2014). Task: Shock Wave Laminar Boundary Layer Interactions in Nonequilibrium Hypersonic Flow.

9. HI-LIFT (HIGH LIFT OVER DRAG EARTH RE-ENTRY STRATEGIES FOR EXPLORATION MISSION). European Space Agency ITT. Aerodynamic and Aerothermodynamic performances analysis. Aerodynamic and Aerothermodynamic databases development.

10. HEXAFLY-INT (HIGH-SPEED EXPERIMENTAL FLY VEHICLES). Seventh Framework Programme. Aerodynamic and aerothermodynamic design of an advanced waverider derived configuration.

11. MARS-GET (MARS ROBOTIC EXPLORATION PROGRAM-2 - PRELIMINARY DESIGN AND PERFORMANCE VERIFICATION OF CRITICAL ELEMENTS FOR GUIDED ENTRY THRUSTERS). European Space Agency ITT. Aerodynamic and aerothermodynamic analysis of thrust effects for precision landing on Mars.

12. MINIRENE. European Space Agency. Aerodynamic design of a capsule with deployable heat shield for a sounding rocket flight experiment.

13. DOC (DEMISE OBSERVATION CAPSULE). European Space Agency. Aerodynamic design of a demise observation capsule.

giuseppe pezzella cv-itadidattica.cressi.unicampania.it/cv/057047-it.pdf · 2020. 8. 31. · (anno...

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