PUBLICATIONS

 JOURNAL ARTICLES

1. Using Aluminum For Space Propulsion, AIAA Journal of Propulsion and Power

Vol. 20; No. 6, November-December 2004, pp. 1056 -1063, ISSN: 0748-4658, doi: 10.2514/1.5132.

A. Ingenito, C. Bruno (2004),

2. “Supersonic Mixing And Combustion: Advance In LES Modeling”,

In: Luigi De Luca; Christophe Bonnal; Oskar Haidn; Sergey M. Frolov. Eucass Book Series, Advances In Aerospace Sciences- Propulsion  Physics. Vol. 1, P. 471-486, Moscow: Torus Press

 A. Ingenito, C. Bruno;

3. “Turbulent Combustion Modeling in Supersonic Flows for Future RBCC Vehicles”, 

 Transactions of the Japan Society for Aeronautical and Space Sciences, Space Technology Japan, Vol. 7, No. ISTS26, pp. 71-76; 1347-3840

 A. Ingenito, C. Bruno;

4. “Physics and Regimes in Supersonic Combustion”,

 AIAA Journal. Volume 48, Number 3, March 2010, pp. 515-525, doi: 10.2514/1.43652.

 A. Ingenito, C. Bruno, 

5. “Preliminary Sizing of Hypersonic Airbreathing Airliner”,

 Transactions of the Japan Society for Aeronautical and Space Sciences, Space Technology, Vol. 8, No. ISTS27, pp. 19- 28, 2010, Japan. 1884-0485

A. Ingenito, C. Bruno,  S. Gulli, 

6. “Sizing of a Scramjet Vehicle”, 

 accepted for publication in  EUCASS Propulsion Physics book,  by Luigi De Luca, Pr. Oskar Haidn, Pr. A.     

 Frolov and Bonnal Christophe, Vol. 2, 2010. ISBN:978-2-7598-0411-5

 A. Ingenito, S. Gulli, C. Bruno, 

7. “Sizing of a fully integrated Hypersonic Commercial Airliner”,

 AIAA Journal of Aircraft, Vol. 48, No. 6 (2011), pp. 2161-2164, doi: 10.2514/1.C000205.

 A. Ingenito, S. Gulli,  C. Bruno, G. Colemann, B. Chudoba and P. A. Czysz,

8. “Hydrogen/air supersonic combustion for future hypersonic vehicles”,

International Journal of Hydrogen Energy, Volume 36, Issue 18, September 2011, Pages 11969-11984, doi: 10.1016/j.ijhydene.2011.06.051;

D. Cecere, A. Ingenito, E. Giacomazzi, L. Romagnosi, C. Bruno

9. “Fuel Consumption Reduction and Weight Estimate of an Intercooled-Recuperated Turboprop Engine”,

 International Journal of Turbo & Jet-Engines, Volume 29, Issue 3, Pages 165–177, ISSN (Online) 2191-0332, ISSN (Print) 0334-0082,  

 DOI: 10.1515/tjj-2012-0025, September 2012;

 R.  Andriani, U. Ghezzi,  A. Ingenito, F. Gamma,

10. “Large Eddy Simulation of Turbulent Hydrogen-fuelled Supersonic Combustion in an Air Cross-Flow”,

 Shock Waves Pages 1-14, ISSN: 09381287, DOI: 10.1007/s00193-013-0454-7, 2013;

 A. Ingenito, D. Cecere, E. Giacomazzi;

11. “Performance of a Turboprop Engine with Heat Recovery in Off-Design Conditions".

 Int. J. Turbo Jet-Engines, Volume 0, Issue 0, Pages 1–11, ISSN (Online) 2191-0332, ISSN (Print) 0334-0082, DOI: 10.1515/tjj-2013-

 0023, September 2013. 

 Roberto Andriani,  Umberto  Ghezzi, Fausto Gamma,  Antonella Ingenito, Antonio Agresta,. 

12. “A review on hydrogen industrial aerospace applications” , 

 International Journal of Hydrogen Energy.Volume 39, Issue 20, Pages 10731-10747, ISSN: 03603199, 2014.

 Cecere, D. , Giacomazzi, E., Ingenito, A.   

13. “NOx Reduction Strategies For Hydrogen Fuelled Aviation Vehicles”,

 International Journal of Hydrogen Energy.(ISSN:1879-3487), 2015;

 Antonella Ingenito, A. Agresta, Roberto Andriani,  Fausto Gamma, 

14. “Theoretical Investigation of Air vitiation effects on hydrogen fuelled Scramjet performance”,

International Journal of Hydrogen Energy. (ISSN:1879-3487), 2015;

Antonella Ingenito

15. NOx reduction strategies in scramjet combustors,

Aerospace Science and Technology,

Ingenito, A.,  59, pp. 189-198, DOI: 10.1016/j.ast.2016.10.020, (www.scopus.com).

16. "Experimental study of pyrolysis–combustion coupling in a regeneratively cooled combustor: System dynamics analysis", 

Aerospace Science and Technology, 67, pp. 473-483, DOI: 7,10.1016/j.ast.2017.04.026, 2017l.

Taddeo, L., Gascoin, N., Chetehouna, K., Ingenito, A., Stella, F., Bouchez, M., Le Naour, B.,

17. Impact of hydrogen fueled hypersonic airliners on the O3 layer depletion, (2018)

International Journal of Hydrogen Energy,

Ingenito, A., pp. 22694-22704, DOI: 10.1016/j.ijhydene.2018.09.208.

18. Experimental study of pyrolysis-combustion coupling in a regeneratively cooled combustor: Heat transfer and coke formation, (2019)

Fuel, 239, pp. 1091-1101, DOI: 10.1016/j.fuel.2018.11.096.

Taddeo, L., Gascoin, N., Chetehouna, K., Ingenito, A., Stella, F., Bouchez, M., Le Naour, B.,

19.  Subsonic Combustion Ramjet Design (2021), 

Springer Briefs in Applied Sciences and Technology, Springer, ISSN: 2191-530X, 2021.

Antonella Ingenito, 

20. The implication of injection locations in an axisymmetric cavity-based scramjet combustor.

ENERGIES, vol. 14, ISSN: 1996-1073, doi: 10.3390/en14092626

Relangi N., Ingenito A., Jeyakumar S. (2021). 

21. Some Key Issues in Hypersonic Propulsion, Energies 2021, 14(12), 3690; https://doi.org/10.3390/en14123690.

Bruno, C., Ingenito, A. (2021), 

22. Review on the Regression Rate-Improvement Techniques and Mechanical Performance of Hybrid Rocket Fuels, FirePhysChem, 2021, ISSN 2667-1344, https://doi.org/10.1016/j.fpc.2021.11.016.

Yash Pal, Sri Nithya Mahottamananda, Sasi Kiran Palateerdham, Sivakumar Subha, Antonella Ingenito,  (2021), 

23. The investigation of inclined aft wall cavities in a circular scramjet combustor,

International Journal of Engine Research, 2022.

Relangi N., Ingenito A., Jeyakumar S., 

24. Combustion performance of hybrid rocket fuels loaded with MgB2 and carbon black additives,

Propulsion and Power Research, 2022, ISSN 2212-540X, https://doi.org/10.1016/j.jppr.2022.11.003.

Yash Pal, Sasi Kiran Palateerdham, Sri Nithya Mahottamananda, Subha Sivakumar, Antonella Ingenito, 

25. Beeswax–EVA/Activated-Charcoal-Based Fuels for Hybrid Rockets: Thermal and Ballistic Evaluation,

Energies, 2022, 15(20), 7578

Mahottamananda, S.N., Pal, Y., Dinesh, M., Ingenito, A., 

26. Thermal decomposition kinetics and combustion performance of paraffin-based fuel in the presence of CeO2 catalyst, 

https://doi.org/10.1016/j.fpc.2022.10.005, FirePhysChem, October 2022

Yash Pal, Sri Nithya Mahottamananda, Subha S, Sasi Kiran Palateerdham, Antonella Ingenito,

27. Array of carbon black-based microthrusters for CubeSat applications

FirePhysChem, FirePhysChem, February 2023, ISSN 2667-1344, https://doi.org/10.1016/j.fpc.2023.01.001.

A Ingenito, SK Palateerdham, M Panzanaro

28. Mars One-Year Mission Craft

Claudio Bruno, Antonella Ingenito, Domenico Simone

Aerospace 2023, 10(7), 610; https://doi.org/10.3390/aerospace10070610 

29. Influence of cavity floor injection strategy on mixing improvement study of a splitter plate-assisted supersonic combustor

Gautam Choubey, Om Patel, Malhar Solanki, Antonella Ingenito, Yuvarajan Devarajan, Sumit Tripathi 

Volume 155, October 2023, Pages 995-1012; Engineering Analysis with Boundary Elements

https://doi.org/10.1016/j.enganabound.2023.07.022 

30. Oxidation reaction kinetics of HTPB-boron carbide/polytetrafluoroethylene formulations as a solid fuel

Yash Pal a, Sri Nithya Mahottamananda b, Sasi Kiran Palateerdham c, Antonella Ingenito c, Djalal Trache d

Fuel, Volume 352, 15 November 2023, 129042

https://doi.org/10.1016/j.fuel.2023.129042

CONFERENCE PAPERS

1. Catalysis and Cracking for Microrocket Application,

E. Giacomazzi, A. Ingenito and C.Bruno, ISTS Paper 2004-b-45,

In Proceedings of the 24th Int. Symp. on Space Technology and  Science,

ISTS web papers archives, pp. 246-251, Miyazaki, Japan, May 30-June 2, 2004.

2. LES of Supersonic Combustion of H2/vitiated air,

A. Del Rossi, A. Ingenito, V. Parisi, E. Giacomazzi and C. Bruno, AIAA Paper 2004-3877,

40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Fort Lauderdale, Florida, 11-14 July 2004.

3. LES Modelling of Scramjet Combustion,

A. Ingenito, G. De Flora, E. Giacomazzi, C. Bruno and Johan Steelant, AIAA paper 2006-1383,

44th  AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 9-12 January 2006.

4. A Novel Model of Turbulent Supersonic Combustion: Development and Validation

A. Ingenito, G. De Flora, E. Giacomazzi, C. Bruno and Johan Steelant,

AIAA paper 2006-4351, 42nd  AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Sacramento, California, 9 - 12 Jul 2006.

5. Supersonic Combustion: Modelling and Simulations

A. Ingenito, E. Giacomazzi, C. Bruno and Johan Steelant, AIAA paper 2006-7962,

14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, Canberra, Australia, 6-9 November 2006.

6. Advance in Supersonic Combustion Modeling and Simulations

A. Ingenito, C. Bruno and Johan Steelant, paper AIAA-2007-0837,

45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 8-11 January 2007.

7. Advance in LES Modelling: Effect of the Turbulent Schmidt Number on Supersonic Regime

A Ingenito, C. Bruno, AIAA paper 2007-5633,

43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cincinnati, OH, 8-11 July 2007. In: Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Vol.  6, pp. 6162-6170, 2007

8. Effect of the Turbulent Schmidt Number on Supersonic Regime

A. Ingenito, C. Bruno, paper ISABE-2007-1312, XVIII ISABE CONFERECE, 2-7 September 2007, Beijing, China.

18th ISABE, AIAA, Reston, VA, 2007, ISBN-10: 1-56347-931-1, ISBN-13: 978-1-56347-931-1

9. LES of a Supersonic Combustor with Variable Turbulent Prandtl and Schmidt Numbers

A. Ingenito and C. Bruno, AIAA-2008-0515,

47th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 7-11 January 2008.

10. LES of Supersonic combustion with a variable turbulent Schmidt Number

A. Ingenito and C. Bruno, AIAA-2008-2586,

15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Dayton, Ohio, Apr. 28-1, 2008.

11. Mixing and Combustion in Supersonic Reactive Flows

A. Ingenito and C. Bruno, AIAA-2008-4574,

44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Hartford, CT, July 21-23, 2008.

12. Reaction Regimes In Supersonic Combustion

A. Ingenito, C. Bruno, Aiaa-2009-0812, 

47th AIAA Aerospace Sciences Meeting and Exhibit. Orlando, Florida, 5-8 January 2009.

13. Sizing of Scramjet Vehicles

A. Ingenito, S. Gulli and C. Bruno,

3rd EUCASS Conference, Versailles, 6-9 July 2009;

14. Sizing of TBCC Hypersonic Airbreathing Vehicles

A. Ingenito, S. Gulli, C. Bruno, AIAA-2009-5186,

45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Denver, Colorado, Aug. 2-5, 2009;

15. TBCC Hypersonic Performance: Effect of Inlet Entropy

A. Ingenito, S. Gulli, C. Bruno, AIAA-2009-7419,

16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, Oct. 19-22, 2009;

16. LES of the HyShot scramjet combustor

A. Ingenito, C. Bruno and D. Cecere, AIAA paper 2010-0758,

48th Aiaa Aerospace Sciences Meeting and Exhibit;  Orlando, Florida, AIAA-2010-758,  4-7 January 2010;

17. Sizing of a Ramjet Powered Vehicle for Mars Exploration

A. Ingenito, C. Bruno, P. Czysz; paper SP2010_1842397,

ESA-3AF Space Propulsion 2010, San Sebastian, 3 - 6 May 2010;

18. Advances in LES of the HyShot II Scramjet Combustor

D. Cecere, A. Ingenito, C. Bruno, E. Giacomazzi, F. Donato, 

XXXIII Event of the Italian Section of the CI and Second S4FE, June, 27-30 - 2010, ISBN 978-88-88104-11-9, doi:10.4405/ptse2010.II1.

19. RANS Study of Hydrogen-Air Turbulent Non-Premixed Flames

D. Daniele, E. Giacomazzi, C.  Bruno, A. Ingenito,

In Proceeding of XXXIII Event of the Italian Section of the CI and Second S4FE, June, 27-30 – 2010,

ISBN 978-88-88104-11-9, doi:10.4405/ptse2010.P1.5.

20. Supersonic combustion regime: numerical and theoretical study,

A. Ingenito, D. Cecere, E. Giacomazzi,

In proceeding of XXXIV Event of the Italian Section of the CI, doi: 10.4405/34proci2011.II13.

21. Prediction of SCRJ flame anchoring

A. Ingenito, D. Cecere and C. Bruno,

In: Proceeding of Second Sino-Italian Conference on Space Aerothermodynamics And Hot Structures, Italy, 6th - 8th July 2010.

22. Shock/Boundary Layer/Heat Release Interaction in the HyShot II Scramjet Combustor

D. Cecere, A. Ingenito, L. Romagnosi, C. Bruno, E. Giacomazzi, AIAA-2010-7066,

In: Proceeding of 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Nashville, Tennessee, July 25-28, 2010.

23. Hypersonic vehicles powered by environmental atmosphere ramjet for Mars exploration

A. Ingenito, C. Bruno, P. Czysz,

In proceeding of  61st International Astronautical Congress, Prague, Czech Republic. Sept. 29 – Oct.1, 2010.

24. The role of the baroclinic term in fuel/air mixing enhancement

L. Romagnosi, A. Ingenito, D. Cecere, E. Giacomazzi, C. Bruno, AIAA paper 2011-0758,

In proceeding of 49th AIAA Aerospace Sciences Meeting and Exhibit;  Orlando, Florida, 4-7 January 2011;

25. Mixing and turbulent kinetic Energy scaling in compressible reacting flows

L. Romagnosi, A Ingenito, D. Cecere, E. Giacomazzi, C. Bruno,

In Proceeding of 17th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference,

AIAA-2011-2364, San Francisco, USA, 2011; ISBN: 978-1-60086-942-6, DOI: 10.2514/MHYTASP11

26. LAPCAT II : conceptual design of a Mach 8 TBCC civil aircraft, enforced by full Navier-Stokes 3D nose-to-tail computation

Sebastien Defoort, Marc Ferrier, Laurent Serre, Dominique Scherrer, Christophe Paridaens, Patrick Hendrick, Antonella Ingenito and Claudio Bruno,

AIAA-2011-2317, 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference , San Francisco, California, Apr. 11-14, 2011, 978-1-60086-942-6

27. LAPCAT II : conceptual design of a Mach 8 TBCC civil aircraft

Sébastien DEFOORT,  Marc FERRIER, Dominique SCHERRER, Laurent SERRE, Christophe PARIDAENS, Patrick HENDRICK, Antonella INGENITO, Claudio BRUNO,

4TH EUROPEAN CONFERENCE FOR AEROSPACE SCIENCES (EUCASS), Saint Petersburg, Russia,  4 –  8, July 2011;

28. Turbulence Scaling in Supersonic Flows

Antonella Ingenito and Claudio Bruno, 28th ISTS, 5-12 June 2011, Japan.

29. Aeronautical approach and support to Mars Exploration

C. Bruno, A. Ingenito, D. Simone, P. Czysz , J. W. Lee,

Proceeding of 47th JPC Conference, Paper No. AIAA-2011-5724, 2 August 2011, San Diego (CA), 978-1-60086-949-5,

DOI: 10.2514/6.2011-5724

30. Theoretical and Numerical analysis of the Turbulence scaling in Supersonic Flows

A. Ingenito, D. Cecere, E. Giacomazzi, C. Bruno, Paper no. AIAA-2011-5919,

Invited, 47th JPC Conference, 2 Augut 2011, San Diego, CA , 978-1-60086-949-5.

31.  Numerical and Theoretical Study of Supersonic Turbulent Non premixed flames

A. Ingenito, L. Romagnosi, D. Cecere, E. Giacomazzi and C. Bruno, ISABE-2011-1535, September 12-16, 2011, Göteborg, Sweden,

ISBN 9781618391803;

32. Supersonic combustion regime: Numerical and theoretical study

A. Ingenito, D. Cecere, E. Giacomazzi, Italian Session of the Combustion Institute, 24-26 October, 2011, ISBN 978-88-88104-11-9.

33. Supersonic Turbulent Non premixed flames: Numerical and Theoretical Study

A. Ingenito, L. Romagnosi, D. Cecere, E. Giacomazzi and C. Bruno,

3th Sino-Italian Conference on Space Aerothermodynamics and Hot Structures, Shanghai · China, November 21-23, 2011.

34. Non-Premixed Supersonic Flames: Combustion Models

A. Ingenito, D. Cecere, E. Giacomazzi, C. Bruno, AIAA paper 2012-0758,

50th Aiaa Aerospace Sciences Meeting and Exhibit;  Orlando, Florida, 9-12 January 2012, ISBN: 978-1-60086-936-5,

DOI: 10.2514/MASM12

35. A comparative study of combustion between biofuels and fossil fuels

A. Ingenito, R. Andriani, A. Agresta, F. Gamma,

10th Annual International Energy Conversion Engineering Conference, 29 July - 1 August 2012, Atlanta, Georgia,

ISBN: 978-1-62410-190-8, DOI: 10.2514/MIECEC12.

36. Numeric Simulation of a Gas Turbine Engine With Constant Volume Combustion,

R. Andriani, A. Ingenito, F. Gamma, A. Agresta,

10th Annual International Energy Conversion Engineering Conference, 29 July - 1 August 2012, Atlanta, Georgia,

ISBN: 978-1-62410-190-8, DOI: 10.2514/MIECEC12.

37. Thermodynamic Characteristics of a Turboprop Engine with Heat Exchangers for Unmanned Aerial Vehicles,

Roberto Andriani, Antonella Ingenito, Fausto Gamma, Antonio Agresta,

51st AIAA Aerospace Sciences Meeting, January 2013, DOI: 10.2514/6.2013-114

38. Off-Design Characteristics of Low-Fuel Consumption Gas Turbine Engine for Long-Range UAV (AIAA 2013-3630)

Roberto Andriani, Umberto Ghezzi, Antonella Ingenito, Fausto Gamma, Antonio Agresta,

49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 2013, DOI: 10.2514/6.2013-3630

39. Air vitiation effects in scramjet engines (AIAA 2013-3701)

Antonella Ingenito, Antonio Agresta, Roberto Andriani, Fausto Gamma,

49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 2013, DOI: 10.2514/6.2013-3701

40. Laminar flame speed of Fossil/Air and Biofuels/Air Combustion (AIAA 2013-3739)

Antonella Ingenito, Roberto Andriani, Antonio Agresta, Fausto Gamma,

11th International Energy Conversion Engineering Conference, July 2013, DOI: 10.2514/6.2013-3739

41. Low-Fuel Consumption Gas Turbine Engines for Extended-Range UAVs,

Roberto Andriani, Antonella Ingenito, Fausto Gamma, Antonio Agresta, January 2014,

52nd Aerospace Sciences Meeting, doi: 10.2514/6.2014-1315

42. RQL combustion as an effective strategy to NOX reduction in gas turbine engines,

Antonella Ingenito, Antonio Agresta, Fausto Gamma, Roberto Andriani (2014) 

November 14-20, MONTREAL, CANADA, 2014

43. Low-Fuel Consumption Gas Turbine Engines for Extended-Range UAVs,

R. Andriani; A. Ingenito; F. Gamma; A. Agresta (2014) 

52nd Aerospace Sciences Meeting. 52nd Aerospace Sciences Meeting, 2014

44. Electrochemical propulsion for space exploration. AIAA 2015-0161

Alessandro Bellomo, Antonella Ingenito, Antonio Agresta, Fausto Gamma, Claudio Bruno

Kissimmee, Florida, 53rd Aerospace Sciences Meeting

45. Preliminary analysis of strategies for NOx reduction

Antonella Ingenito, Antonio Agresta, Roberto Andriani, Fausto Gamma

AIAA SciTech AIAA 2015-0885 01/2015 Kissimmee, Florida, 53rd Aerospace Sciences Meeting

46. Feasibility of high speed atmospheric flight on Venus.

Lorenzo Toro, Antonella Ingenito, Antonio Agresta, Roberto Andriani, Fausto Gamma, Claudio Bruno 

Kissimmee, Florida, 8th Symposium on Space Resource Utilization.

47. Experimental Investigation of Fuel Cooled Combustor,

L Taddeo, N Gascoin, K Chetehouna, A Ingenito, F Gamma, M Bouchez, , Bruno Le Naour 

52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016

48. Experimental Investigation of Fuel-Cooled Combustor: Cooling Efficiency and Coke Formation

Lucio Taddeo, Nicolas Gascoin, Khaled Chetehouna, Antonella Ingenito, Fulvio Stella, Marc Bouchez, Bruno Le Naour

21st AIAA International Space Planes and Hypersonics Technologies Conference, 2017

49. Thermal analysis and performance of a pressure gain combustion system

Roberto Andriani, Antonella Ingenito, A. Agresta

Proceedings of the 7th European Conference for Aeronautics and Space Sciences (EUCASS), 2018, Milan, Italy

50. Numerical and Experimental Study of a 200 N Paraffin/N2O hybrid rocket

Sachin Srivastava,  Antonella Ingenito, Roberto Andriani

EUCASS 2019-8th European Conference for Aeronautics and Space Sciences, 2019

51. Main Performances of the Unsteady Constant Volume Combustion Thermodynamic Cycle

Roberto Andriani, Antonella Ingenito

EUCASS 2019-8th European Conference for Aeronautics and Space Sciences, 1-6, 2019

52. Theoretical and Experimental investigation of a low thrust Paraffin/N2O hybrid rocket

Sachin Srivastava,  Antonella Ingenito, Roberto Andriani,

AIAA Propulsion and Energy 2019 Forum, 2019.

53. A hybrid propulsion solution for a microsatellite to perform a capture maneuver in a mars orbit,

Domingos, C.H.F.L., Ingenito, A.

AIAA Propulsion and Energy 2020 Forum, 2020, pp. 1–17

54. Numerical simulations of axisymmetric aft wall angle cavity in supersonic combustion ramjets,

Relangi, N., Garimella, D., Jayaraman, K., ...Jeyakumar, S., Ingenito, A.

AIAA Propulsion and Energy 2020 Forum, 2020, pp. 1–15

55. Design and experimental set-up of a paraffin based hybrid rocket engine to brake a 24U microsatellite in a Mars orbit,"

Domingos, Caio Henrique Franco Levi; Palateerdham, Sasi Kiran; Ingenito, Antonella; Vecchio, Stefano; ,

5th IAA Conference on University Missions and CubeSat Workshop, Rome", 2020

Advances in the Astronautical Sciences, 2020, 173, pp. 545–561, AAS 20-257;

56. Mission analysis in the braking effect of a small microsatellite using a hybrid rocket engine to achieve a mars orbit,

Ferreira, R.S., Domingos, C.H.F.L., Ingenito, A., Teofilatto, P.

Advances in the Astronautical Sciences, 2020, 173, pp. 335–348, AAS 20-230;

57. Experimental and numerical investigation of a paraffin-based hybrid rocket engine to brake a 24U microsatellite in a Mars orbit,

Domingos, C.H.F.L., Ingenito, A., Simone, D.

Proceedings of the International Astronautical Congress, IAC, 2020, 2020-October.

58. Numerical analysis of a N2O paraffin fueled hybrid rocket to perform capture maneuvers in a Mars orbit,

Domingos, C.H.F.L., Ingenito, A., Simone, D., Filho, R.B.N.

Proceedings of the International Astronautical Congress, IAC, 2021.

59. Analytical and Numerical Study of the N2O Flow in the Feed System of a Small Satellite,

Do Nascimento Filho, R.D.B., Levi Domingos, C.H.F., Simone, D., Ingenito, A.

Proceedings of the International Astronautical Congress, IAC, 2021

60. Numerical investigations of fuel injection techniques in a cavity-based scramjet,

Relangi, N., Ingenito, A., Jeyakumar, S., Hussain, K.F.

Proceedings of the International Astronautical Congress, IAC, 2021

61. CFD simulations of a N2O/paraffin fueled hybrid rocket to perform capture maneuvers in a Mars orbit

Domingos, C.H.F.L., Ingenito, A., Filho, R.B.D.N., Simone, D,

AIAA Propulsion and Energy Forum, 2021, 2021, AIAA 2021-3522

62. Design of Supersonic and Hybrid engine based Advanced Rocket (SHAR)

Relangi Naresh; Peri L N Phaneendra; Domingos, Caio Henrique F L; Fossella, Amalia; Henriques, Julia Meria Leite; Ingenito, Antonella

IOP Conference Series: Materials Science and Engineering,1226,1,012031, 2022, IOP Publishing

63. Understanding the total pressure losses nature in a Scramjet Combustor (AIAA 2023-3040)

Sasi Kiran Palateerdham, Lakshmi Narayana Phaneendra Peri, Antonella Ingenito, Yash Pal and Sri Nithya Mahottamananda

25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, May 28 - June 1, 2023, India

64. SHAR for a TSTO Launcher

Naresh Relangi, L.N. Phaneendra Peri, Sasi Kiran Palateerdham and Antonella Ingenito

25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, May 28 - June 1, 2023, India

65. Numerical investigation of the impact of injectors location on fuel mixing in the HIFiRE 2 Scramjet combustor

Sasi Kiran Palateerdham*, Lakshmi Narayana Phaneendra Peri, Antonella Ingenito, Ashish Vashishtha

66. Numerical Study of Hydrogen Injection to initiate Oblique Detonation Wave

Ashish Vashishtha, Rushikesh Kore, Sasi Kiran Palateerdham, Antonella Ingenito

The 3rd International Conference on High-Speed Vehicle Science and Technology - April 2024

67. Influence of high-density energetic particles on combustion of solid fuels for Ramjet applications

Sasi Kiran Palateerdham, Abdul Rahman, Sri Nithya Mahottamananda, Yash Pal, Antonella Ingenito

The 3rd International Conference on High-Speed Vehicle Science and Technology - April 2024

68. Investigation of mixing and Combustion in supersonic flows 

Sasi Kiran Palateerdham, Lakshmi Narayana Phaneendra Peri, Antonella Ingenito, Gautam Choubey

The 3rd International Conference on High-Speed Vehicle Science and Technology - April 2024

69. TSTO Launcher for small Satellites

Lakshmi Narayana Phaneendra Peri, Francesco Margani, Luca Armani, Sasi Kiran Palateerdham, Antonella Ingenito

The 3rd International Conference on High-Speed Vehicle Science and Technology - April 2024

70. Knowledge Discovery on Cavity-Based Scramjet Combustor Design via Stochastic-Surrogate-Assisted Multi-Objective Optimization

Chihiro Fujio, Sasi Kiran Palateerdham, Lakshmi Narayana Phaneendra Peri, Hideaki Ogawa, and Antonella Ingenito

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