Salta al contenuto principale
Ricerc@Sapienza
Toggle navigation
Home
Login
Home
Persone
arianna.remiddi@uniroma1.it
Arianna Remiddi
Assegnista di ricerca
Struttura:
DIPARTIMENTO DI INGEGNERIA MECCANICA E AEROSPAZIALE
E-mail:
arianna.remiddi@uniroma1.it
Pagina istituzionale corsi di laurea
Curriculum Sapienza
Pubblicazioni
Titolo
Pubblicato in
Anno
A-posteriori analysis of a data-driven filtered wrinkled flamelet model for thermodiffusively unstable premixed flames
COMBUSTION AND FLAME
2024
Efficient multiphysics simulations of LRE combustion chambers using tabulated chemistry
Proceedings of the 9th Edition of the 3AF International Space Propulsion Conference
2024
Data-driven modeling of resolved and filtered thermo-diffusively unstable hydrogen–air flames
PROCEEDINGS OF THE COMBUSTION INSTITUTE
2024
Dataset of wall-resolved large-eddy simulations turbulent pseudoboiling in cryogenic hydrogen pipe flows
JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER
2023
A pressure-based numerical Framework for highly stratified transcritical real-fluids simulations
AIAA Scitech 2023 Forum
2023
A data-driven approach for hydrogen premixed combustion modeling
Proceedings of the Belgian and Italian Sections of The Combustion Institute
2023
Towards lean premixed hydrogen combustion modelling using a data-driven approach
2023
Heat Transfer in Rocket Combustion Chambers Firing Plates: Role of Injector Confinement
JOURNAL OF PROPULSION AND POWER
2023
Assessment of phase-separation phenomena in LREs cryogenic flows
Aerospace Europe Conference 2023 – 10ᵀᴴ EUCASS – 9ᵀᴴ CEAS
2023
Development and validation of an efficient numerical framework for Conjugate Heat Transfer in Liquid Rocket Engines
AIAA SCITECH 2022 Forum
2022
Dataset of wall-resolved large eddy simulations for the investigation of turbulent pseudo-boiling and wall-functions in cryogenic hydrogen pipe flows
AIAA SCITECH 2022 Forum
2022
Efficient time-resolved thermal characterization of single and multi-injector rocket combustion chambers
PROCEEDINGS OF THE COMBUSTION INSTITUTE
2022
Multi-region thermal characterization in LRE combustion chambers
9ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Proceedings
2022
Characterization of the injectors near-field region of LRE combustion chambers
9ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Proceedings
2022
Validation and development of wall-function models for liquid rocket engine applications
9ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Proceedings
2022
A data driven Filtered Wrinkled Flamelet model for premixed hydrogen-air flames
Combustion for Sustainability
2022
Effects of injector lateral confinement on lre wall heat flux characterization: Numerical investigation towards data-driven modeling
AIAA Scitech 2021 Forum
2021
Application of wall functions approaches in the contextof LRE combustion chambers simulations
AIAA Scitech 2021 Forum
2021
An efficient modeling framework for wall heat flux prediction in rocket combustion chambers using non adiabatic flamelets and wall-functions
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER
2021
Multi-physics modeling of Liquid Rocket Engine combustion chambers
Proceedings of the Italian Section of the Combustion Institute
2021
1
2
seguente ›
ultima »
Progetti di Ricerca
Multi-fidelity numerical investigation of transcritical combustion and heat transfer in Liquid Rocket Engine propulsion systems
Gruppi di ricerca
Modellistica della Combustione
© Università degli Studi di Roma "La Sapienza" - Piazzale Aldo Moro 5, 00185 Roma