SIMONE D'ALESSANDRO

Dottore di ricerca

ciclo: XXXII


supervisore: Francesco Nasuti
relatore: Francesco Nasuti

Titolo della tesi: Low Order Modeling Approach to Longitudinal and Transverse Combustion Instability in Liquid Rocket Engines

High frequency combustion instability in liquid propellant rocket engines arises from the coupling between unsteady heat release rate and acoustics of the combustor. If unpredicted, such kind of instability can often result in the rapid destruction of the engine. From the numerical point of view, two different ways exist to approach the subject: the so-called high-fidelity and low-order models. The former ones, such as LESs or DESs, are capable of giving lots of information on the flow field but still struggle to give an accurate prediction of combustion instability, which would make experiments unnecessary. Moreover, they require a huge computational and economical effort that is prohibitive during the development phases of a new engine. Low-order models, on the other hand, require a larger modeling effort to include suitable laws capable of capturing the physics of the problem, but they are usually fast and cheap in terms of computations and data storage and, as a consequence, in terms of financial requirements. For such reason they deserve attention to be paid in the research community, since a predictive low-order model could represent an useful design tool. The approach which has been developed and is presented in this thesis is a brand new formulation belonging to the family of low-order models. The formulation novelty lies in the simplified heat release to acoustics coupling function, the so- called response function, which is realized here by means of the modeling of the shear-coaxial injector dynamics. In particular, the fuel mass flow rate injected by the elements is linked to the acoustic field here, in the place of linking directly the acoustics to an energy source term, as commonly done in the literature. In order to implement such low-order model a new one-dimensional injector solver is developed from scratch and it is used to solve one-dimensional problems. After that, such solver is even more interestingly used as a “tool” to solve the injectors flow fields within an existing in-house CFD solver, in order to deal with multi-dimensional instability problems. The employed set of equations is Eulerian and a simplified single step chemical mechanism is adopted to solve combustion. The model testing is performed onto two different test-cases, namely the Con- tinuously Variable Resonant Combustor (CVRC) and the Transverse Instability Combustor (TIC), both designed and assembled at Purdue University, IN, USA. CVRC is a single injector system affected by longitudinal combustion instability, while TIC is a multi-element test-engine affected by transverse instability. Prelimi- nary linear acoustics analyses are performed on both systems in order to validate the solver. After that, since the low-order model employs several free parameters, different sensitivity analyses are carried out to assess their role and to set them properly. Such analyses showed how the most part of the free parameters employed in the formulation is in fact negligible, while few of them are important. Finally, the self-excited behaviors of CVRC and TIC are simulated. Outcomes are satisfactorily: the model is capable to predict the high frequency oscillating behaviors of both CVRC and TIC within a low error threshold, provided an appropriate model tuning, which is however independent of the use of external data coming from experiments or other more detailed simulations.

Produzione scientifica

11573/1706427 - 2024 - Low-order modeling approach for the prediction of transverse combustion instabilities in multi-injector engines
Zolla, Paolo Maria; Montanari, Alessandro; D’Alessandro, Simone; Pizzarelli, Marco; Nasuti, Francesco; Pellegrini, Rocco Carmine; Cavallini, Enrico - 01a Articolo in rivista
rivista: CEAS SPACE JOURNAL (Council of European Aerospace Societies) pp. - - issn: 1868-2502 - wos: WOS:001179674800001 (1) - scopus: 2-s2.0-85187169834 (1)

11573/1710421 - 2023 - Driving mechanisms in low-order modeling of longitudinal combustion instability
D'alessandro, S.; Frezzotti, M. L.; Favini, B.; Nasuti, F. - 01a Articolo in rivista
rivista: JOURNAL OF PROPULSION AND POWER (American Institute of Aeronautics & Astronautics:1801 Alexander Bell Drive, Suite 500:Reston, VA 20191:(800)639-2422, (703)264-7500, EMAIL: custserv@aiaa.org, INTERNET: http://www.aiaa.org/, Fax: (703)264-7657) pp. 754-764 - issn: 0748-4658 - wos: WOS:000999458000001 (1) - scopus: 2-s2.0-85184357610 (3)

11573/1697305 - 2023 - Sensitivity Study on a Low Order Model for the Analysis of Transverse Combustion Instability
Montanari, Alessandro; Zolla, Paolo Maria; D’Alessandro, Simone; Pizzarelli, Marco; Nasuti, Francesco; Pellegrini, Rocco Carmine; Cavallini, Enrico - 04b Atto di convegno in volume
congresso: Aerospace Europe Conference 2023 – 10ᵀᴴ EUCASS – 9ᵀᴴ CEAS (Lausanne, Switzerland)
libro: Aerospace Europe Conference 2023 – 10ᵀᴴ EUCASS – 9ᵀᴴ CEAS - ()

11573/1660825 - 2022 - Review and implementation of engineering models of rocket film cooling and nozzle erosion
D'alessandro, Simone; Concio, Pierluigi; Rotondi, Marco; Bianchi, Daniele; Nasuti, Francesco - 04b Atto di convegno in volume
congresso: European conference for aeronautics and space sciences (Lille, Francia)
libro: Proceedings of EUCASS-3AF 2022 - ()

11573/1644024 - 2022 - Student firing tests and launches with commercial and self-made solid rocket motors
Migliorino, M. T.; Aiello, M.; Berti, M.; Rotondi, M.; D'alessandro, S.; Bianchi, D.; Jahjah, M.; Pizzarelli, M. - 01a Articolo in rivista
rivista: ACTA ASTRONAUTICA (Elmsford N.Y.: Pergamon Press) pp. 23-34 - issn: 0094-5765 - wos: WOS:000800589700004 (0) - scopus: 2-s2.0-85130134678 (2)

11573/1667757 - 2022 - Low-order modeling of combustion instability using a hybrid real/ideal gas mixture model
Zolla, Paolo Maria; Montanari, Alessandro; D'alessandro, Simone; Nasuti, Francesco - 04b Atto di convegno in volume
congresso: 9th european conference for aeronautics and space sciences (EUCASS), 2022 (Lille, France)
libro: 9th european conference for aeronautics and space sciences, 2022 - ()

11573/1569484 - 2021 - Film cooling modeling in liquid rocket thrust chambers
Concio, Pierluigi; D'alessandro, Simone; Migliorino, Mario Tindaro; Nasuti, Francesco - 04b Atto di convegno in volume
congresso: AIAA propulsion and energy forum (Virtual, Online)
libro: AIAA propulsion and energy forum - (978-1-62410-611-8)

11573/1547677 - 2021 - Development of a film-cooled thrust chamber component in the ESPSS library
Concio, Pierluigi; D'alessandro, Simone; Nasuti, Francesco - 04b Atto di convegno in volume
congresso: 7th Space Propulsion conference (Rome, Italy)
libro: 7th Space Propulsion conference proceedings - ()

11573/1569480 - 2021 - A hybrid real/ideal gas mixture computational framework to capture wave propagation in liquid rocket combustion chamber conditions
D’Alessandro, Simone; Pizzarelli, Marco; Nasuti, Francesco - 01a Articolo in rivista
rivista: AEROSPACE (Basel : MDPI) pp. - - issn: 2226-4310 - wos: WOS:000699191100001 (1) - scopus: 2-s2.0-85114723140 (1)

11573/1569482 - 2021 - A hybrid real/ideal gas mixture model in the framework of low order modeling of combustion instability
D'alessandro, Simone; Zolla, Paolo Maria; Pizzarelli, Marco; Favini, Bernardo; Nasuti, Francesco - 04b Atto di convegno in volume
congresso: AIAA Propulsion and Energy Forum, 2021 (Evento Virtuale)
libro: AIAA Propulsion and Energy Forum, 2021 - (978-1-62410-611-8)

11573/1644206 - 2021 - Student firing tests and launches with commercial and self-made solid rocket motors
Migliorino, M. T.; Aiello, M.; Berti, M.; Rotondi, M.; D'alessandro, S.; Bianchi, D.; Jahjah, M.; Pizzarelli, M. - 04b Atto di convegno in volume
congresso: IAF Space Propulsion Symposium 2021 at the 72nd International Astronautical Congress, IAC 2021 (Dubai, UAE)
libro: Proceedings of the International Astronautical Congress, IAC - ()

11573/1338852 - 2019 - A low order modeling approach to transverse combustion instability
D'alessandro, Simone; Favini, Bernardo; Nasuti, Francesco - 04b Atto di convegno in volume
congresso: 2019 AIAA Propulsion and energy forum and exposition (Indianapolis, IN; USA)
libro: 2019 AIAA Propulsion and energy forum and exposition - (978-1-62410-590-6)

11573/1339318 - 2019 - Low-order modeling of combustion instability applied to cryogenic propellants
D'alessandro, Simone; Fedeli, Gabriele; Tonti, Federica; Hardi, Justin S.; Oschwald, Michael; Favini, Bernardo; Nasuti, Francesco - 04b Atto di convegno in volume
congresso: 8th European Conference for Aeronautics and Aerospace Sciences (EUCASS) (Madrid; Spain)
libro: Proceedings of the 8th European Conference for Aeronautics and Aerospace Sciences (EUCASS) - ()

11573/1152370 - 2018 - A multi-dimensional approach for low order modeling of combustion instability in a rocket combustor
D'alessandro, Simone; Frezzotti, Maria Luisa; Favini, Bernardo; Nasuti, Francesco - 04b Atto di convegno in volume
congresso: AIAA/SAE/ASEE Joint Propulsion Conference 2018 (Cincinnati, USA)
libro: AIAA/SAE/ASEE joint propulsion conference 2018 - (9781624105708; 9781510869004)

11573/1174487 - 2018 - Low-order modeling of coupling effects between propellant injection and pressure fluctuations in high frequency combustion instability
Frezzotti, M. L.; D’Alessandro, S.; Gallo, G.; Favini, B.; Nasuti, F. - 04b Atto di convegno in volume
congresso: Space Propulsion 2018 (Seville, Spain)
libro: Proceedings of Space Propulsion 2018 - ()

11573/1152449 - 2018 - Driving mechanisms in low order modeling of longitudinal combustion instability
Frezzotti, Maria Luisa; D'alessandro, Simone; Favini, Bernardo; Nasuti, Francesco - 04b Atto di convegno in volume
congresso: AIAA Propulsion and Energy Forum 2018. Held at the AIAA propulsion and energy forum 2018 (Cincinnati, Ohio, USA)
libro: 2018 AIAA/SAE/ASEE joint propulsion conference. Proceedings - (9781624105708; 9781510869004)

11573/1016892 - 2017 - Low order investigation on longitudinal combustion instability in a variable geometry single element combustor
Frezzotti, Maria Luisa; D’Alessandro, S.; Huang, C.; Nasuti, F. - 04b Atto di convegno in volume
congresso: 7 TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) (Milano)
libro: 7 TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) - ()

11573/974144 - 2017 - Numerical issues in modeling combustion instability by quasi-1D Euler equations
Frezzotti, Maria Luisa; D'alessandro, Simone; Favini, Bernardo; Nasuti, Francesco - 01a Articolo in rivista
rivista: INTERNATIONAL JOURNAL OF SPRAY AND COMBUSTION DYNAMICS ([Brentwood] : Multi-Science Publishing, 2009-) pp. 349-366 - issn: 1756-8277 - wos: WOS:000415334400010 (6) - scopus: 2-s2.0-85034609322 (13)

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