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daniele.bianchi@uniroma1.it
Daniele Bianchi
Professore Associato
Struttura:
DIPARTIMENTO DI INGEGNERIA MECCANICA E AEROSPAZIALE
E-mail:
daniele.bianchi@uniroma1.it
Pagina istituzionale corsi di laurea
Curriculum Sapienza
Pubblicazioni
Titolo
Pubblicato in
Anno
Family of Skeletal Reaction Mechanisms for Methane–Oxygen Combustion in Rocket Propulsion
JOURNAL OF PROPULSION AND POWER
2024
Integrated Optimization of a Three-Stage Clustered Hybrid Rocket Launcher using Neural Networks
AIAA SciTech Forum 2024
2024
Computational Analysis and Regression Laws for Nozzle Erosion Prediction in Hybrid Rockets
JOURNAL OF PROPULSION AND POWER
2024
Modeling and Analysis of Film Cooling in Oxygen-Kerosene Rocket Thrust Chambers
AIAA SciTech Forum 2024
2024
Radiative Wall Heat Transfer Evaluation in Hybrid Rocket Thrust Chambers
AIAA SciTech Forum 2024
2024
Multi-disciplinary optimization of single-stage hybrid rockets for lunar ascent
ACTA ASTRONAUTICA
2024
Computational Analysis of High-Altitude Test Facilities
Space Propulsion Conference 2024
2024
Experimental Investigation of a H2O2 Hybrid Rocket with Different Swirl Injections and Fuels
APPLIED SCIENCES
2024
NUMERICAL ACTIVITIES ON THE PARAFFIN-BASED FUEL MTM IN THE FRAMEWORK OF THE PHAEDRA PROJECT
Proceedings of the 2024 Space Propulsion Conference
2024
Conjugate heat transfer numerical simulations of a methane-oxygen liquid rocket engine
Proceedings of the 2024 Space Propulsion Conference
2024
Numerical Modeling of Scale Effects in Paraffin-Hydrogen Peroxide Hybrid Rockets with Swirl Injection
Proceedings of the International Astronautical Conference
2024
Multi-disciplinary Optimization of Single-stage Hybrid Rocket with Swirl Injection for Lunar Ascent
AIAA Scitech 2023 Forum
2023
Multiphase Effects on Solid Rocket Nozzle Performance
JOURNAL OF PROPULSION AND POWER
2023
Numerical Simulations of a Paraffin-Hydrogen Peroxide Hybrid Rocket with Swirl Injection
Proceedings of the AIAA Scitech 2023 Forum
2023
Numerical Analysis of Film Cooling and Mixture Ratio Bias in Oxygen-Methane Liquid Rocket Engines
AIAA Scitech 2023 Forum
2023
Role of Finite-Rate Kinetics on the Performance Predictions of Solid Rocket Motor Nozzles
AIAA SciTech Forum 2023
2023
Cooling system design for an upper-stage aerospike
Proceedings of the 34th ISTS Conference
2023
Cooling system analysis of a clustered module aerospike for upper-stage applications
Proceedings of Aerospace Europe Conference 2023 – 10ᵀᴴ EUCASS – 9ᵀᴴ CEAS
2023
Numerical and experimental analysis of fuel regression rate in a lab-scale hybrid rocket engine with swirl injection
AEROSPACE SCIENCE AND TECHNOLOGY
2023
Modeling of swirl injection effects in a H2O2-HDPE hybrid rocket
Proceedings of the Aerospace Europe Conference 2023 - 10th EUCASS - 9th CEAS
2023
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