Junhua Bai, Jiajia Yang, Nan Zhang, Yu Ren & Jie Pan. (2023) The artificial roughness effect on the thermal performance of a submerged combustion vaporizer. Applied Thermal Engineering, pages 121902.
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Paolo Maria Zolla, Matteo Fiore, Pasquale Eduardo Lapenna, Daniele Bianchi & Francesco Nasuti. (2022) A design strategy for water-based noise suppression systems in liquid rocket engines firing tests. CEAS Space Journal 15:4, pages 597-611.
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Hisham Elmouazen, Xiaobing Zhang, Mohammednour Gibreel & Mozdalifah Ali. (2022) Heat transfer enhancement of hydrogen rocket engine chamber wall by using V-shape rib. International Journal of Hydrogen Energy 47:16, pages 9775-9790.
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Shibin Luo, Dequan Xu, Jiawen Song & Jian Liu. (2021) A review of regenerative cooling technologies for scramjets. Applied Thermal Engineering 190, pages 116754.
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M. K. Sahu, Kumari Ambe Verma & K. M. Pandey. 2021. Recent Advances in Mechanical Engineering. Recent Advances in Mechanical Engineering
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Mario Tindaro Migliorino, Daniele Bianchi & Francesco Nasuti. (2020) Numerical Analysis of Paraffin-Wax/Oxygen Hybrid Rocket Engines. Journal of Propulsion and Power 36:6, pages 806-819.
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Xin Li, Silong Zhang, Jiang Qin & Wen Bao. (2020) Parametric analysis on the thermal behavior of cracking hydrocarbon fuel flow inside asymmetry heated cooling channels with micro-ribs. International Journal of Heat and Mass Transfer 160, pages 120154.
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Mario Tindaro MigliorinoDaniele BianchiFrancesco Nasuti. (2020) A Sensitivity Study on a CFD Model for Paraffin-based Hybrid Rockets. A Sensitivity Study on a CFD Model for Paraffin-based Hybrid Rockets.
Daniele BianchiMario Tindaro MigliorinoFrancesco NasutiMarcello Onofri. (2019) CFD Analysis of Paraffin-Based Hybrid Rockets with Coupled Nozzle Erosion Characterization. CFD Analysis of Paraffin-Based Hybrid Rockets with Coupled Nozzle Erosion Characterization.
Mario Tindaro MigliorinoDaniele BianchiFrancesco Nasuti. (2019) Predictive CFD Model for Internal Ballistics of Hybrid Rocket Engines using Supercritical Paraffin-wax and Oxygen. Predictive CFD Model for Internal Ballistics of Hybrid Rocket Engines using Supercritical Paraffin-wax and Oxygen.
Daniele Bianchi, Giuseppe Leccese, Francesco Nasuti, Marcello Onofri & Carmine Carmicino. (2019) Modeling of High Density Polyethylene Regression Rate in the Simulation of Hybrid Rocket Flowfields. Aerospace 6:8, pages 88.
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Giuseppe Leccese, Daniele Bianchi, Francesco Nasuti, Keith Javier Stober, Pavan Narsai & Brian Joseph Cantwell. (2019) Experimental and numerical methods for radiative wall heat flux predictions in paraffin–based hybrid rocket engines. Acta Astronautica 158, pages 304-312.
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D. Bianchi, F. Nasuti & D. Delfini. (2019) Modeling of gas–surface interface for paraffin-based hybrid rocket fuels in computational fluid dynamics simulations. Modeling of gas–surface interface for paraffin-based hybrid rocket fuels in computational fluid dynamics simulations.
Giuseppe LecceseDaniele BianchiFrancesco Nasuti. (2018) Numerical Investigation on the Role of Thermal Radiation in Hybrid Rocket Fuel Pyrolysis. Numerical Investigation on the Role of Thermal Radiation in Hybrid Rocket Fuel Pyrolysis.
Giuseppe LecceseDaniele BianchiFrancesco Nasuti. (2018) Modeling and Simulation of Paraffin–Based Hybrid Rocket Internal Ballistics. Modeling and Simulation of Paraffin–Based Hybrid Rocket Internal Ballistics.
Giuseppe Leccese, Daniele Bianchi, Barbara Betti, Diego Lentini & Francesco Nasuti. (2018) Convective and Radiative Wall Heat Transfer in Liquid Rocket Thrust Chambers. Journal of Propulsion and Power 34:2, pages 318-326.
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Giuseppe LecceseDaniele BianchiFrancesco NasutiKeith J. Stober, Pavan Narsai & Brian J. Cantwell. (2017) Simulations of Paraffin-Based Hybrid Rocket Motors and Comparison with Experiments. Simulations of Paraffin-Based Hybrid Rocket Motors and Comparison with Experiments.
Kunlin Cheng, Yu Feng, Yuguang Jiang, Silong Zhang, Jiang Qin, Duo Zhang & Wen Bao. (2017) Thermodynamic analysis for recuperation in a scramjet nozzle with wall cooling. Applied Thermal Engineering 121, pages 153-162.
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Maria Luisa FrezzottiFrancesco NasutiCheng Huang & William E. Anderson. (2017) Extraction of response function from numerical simulations and their use for longitudinal combustion intsbility modeling. Extraction of response function from numerical simulations and their use for longitudinal combustion intsbility modeling.
Emanuele Martelli, Barbara Betti, Francesco Nasuti & Marcello Onofri. 2017. 30th International Symposium on Shock Waves 1. 30th International Symposium on Shock Waves 1
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Giuseppe Leccese, Daniele Bianchi & Francesco Nasuti. (2016) Modeling of Paraffin-Based Fuels in the Simulation of Hybrid Rocket Flowfields. Modeling of Paraffin-Based Fuels in the Simulation of Hybrid Rocket Flowfields.
Daniele Bianchi, Francesco Nasuti & Carmine Carmicino. (2016) Hybrid Rockets with Axial Injector: Port Diameter Effect on Fuel Regression Rate. Journal of Propulsion and Power 32:4, pages 984-996.
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Barbara Betti, Daniele Bianchi, Francesco Nasuti & Emanuele Martelli. (2016) Chemical Reaction Effects on Heat Loads of CH4/O2 and H2/O2 Rockets. AIAA Journal 54:5, pages 1693-1703.
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Daniele Bianchi, Francesco Nasuti & Carmine Carmicino. (2015) Numerical Analysis of Port Diameter Effect on Hybrid Rocket Fuel Regression Rate with Axial Injection. Numerical Analysis of Port Diameter Effect on Hybrid Rocket Fuel Regression Rate with Axial Injection.
Barbara Betti, Daniele Bianchi, Giuseppe Leccese, Diego Lentini & Francesco Nasuti. (2015) Convective and Radiative Contributions to Wall Heat Transfer in Liquid Rocket Engine Thrust Chambers. Convective and Radiative Contributions to Wall Heat Transfer in Liquid Rocket Engine Thrust Chambers.
Daniele Bianchi, Barbara Betti, Francesco Nasuti & Carmine Carmicino. (2015) Simulation of Gaseous Oxygen/Hydroxyl-Terminated Polybutadiene Hybrid Rocket Flowfields and Comparison with Experiments. Journal of Propulsion and Power 31:3, pages 919-929.
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Barbara Betti, Daniele Bianchi, Francesco Nasuti & Emanuele Martelli. (2014) Chemical Reaction Effects on Wall Heat Flux in Liquid Rocket Thrust Chambers. Chemical Reaction Effects on Wall Heat Flux in Liquid Rocket Thrust Chambers.
Daniele Bianchi, Barbara Betti, Francesco Nasuti, Carmine Carmicino & Annamaria Russo Sorge. (2014) Numerical Modeling of GOX/HTPB Hybrid Rocket Flowfields and Comparison with Experiments. Numerical Modeling of GOX/HTPB Hybrid Rocket Flowfields and Comparison with Experiments.