Paolo Maria Zolla | Ricerc@Sapienza

Pubblicazioni

Titolo	Pubblicato in	Anno
Low-Order Modeling of Combustion Instability: A Comprehensive Analysis of the BKD Test Case	AIAA SciTech Forum 2024	2024
Integrated Optimization of a Three-Stage Clustered Hybrid Rocket Launcher using Neural Networks	AIAA SciTech Forum 2024	2024
Low-order modeling approach for the prediction of transverse combustion instabilities in multi-injector engines	CEAS SPACE JOURNAL	2024
Multi-disciplinary optimization of single-stage hybrid rockets for lunar ascent	ACTA ASTRONAUTICA	2024
Multi-disciplinary Optimization of Single-stage Hybrid Rocket with Swirl Injection for Lunar Ascent	AIAA Scitech 2023 Forum	2023
Sensitivity Study on a Low Order Model for the Analysis of Transverse Combustion Instability	Aerospace Europe Conference 2023 – 10ᵀᴴ EUCASS – 9ᵀᴴ CEAS	2023
Surrogate Neural Network Model for Integrated Ascent Trajectory Optimization of Throttleable Hybrid Rockets	Proceedings of the International Astronautical Congress, IAC	2023
T(H)RUST: applied research activities on liquid rocket propulsion at Sapienza University of Rome	Proceedings of the International Astronautical Congress, IAC	2023
A design strategy for water-based noise suppression systems in liquid rocket engines firing tests	CEAS SPACE JOURNAL	2022
Surrogate neural network for rapid flight performance evaluation of hybrid rocket engines	JOURNAL OF SPACECRAFT AND ROCKETS	2022
Low-order modeling of combustion instability using a hybrid real/ideal gas mixture model	9th european conference for aeronautics and space sciences, 2022	2022
A Hybrid Real/Ideal Gas Mixture Model in the Framework of Low Order Modeling of Combustion Instability	Proceedings of AIAA Propulsion and Energy Forum 2021	2021
Machine Learning Techniques for Flight Performance Prediction of Hybrid Rocket Engines	AIAA Propulsion and Energy Forum, 2021	2021
A Computational Tool for the Design of Hybrid Rockets	AEROTECNICA MISSILI & SPAZIO	2021