Francesco Nasuti

About Francesco Nasuti

Francesco Nasuti, With an exceptional h-index of 37 and a recent h-index of 26 (since 2020), a distinguished researcher at Sapienza Università di Roma, specializes in the field of Aerospace Propulsion.

His recent articles reflect a diverse array of research interests and contributions to the field:

Low-order modeling approach for the prediction of transverse combustion instabilities in multi-injector engines

Design and Evaluation of Aerospike Nozzles for an Upper-Stage Application

Family of Skeletal Reaction Mechanisms for Methane–Oxygen Combustion in Rocket Propulsion

Radiative Wall Heat Transfer Evaluation in Hybrid Rocket Thrust Chambers

Modeling and Analysis of Film Cooling in Oxygen-Kerosene Rocket Thrust Chambers

Low-Order Modeling of Combustion Instability: A Comprehensive Analysis of the BKD Test Case

Transient Analysis of Liquid Rocket Engine Chilldown and Startup by Conjugate Heat Transfer Approach

Conjugate heat transfer applied to transitory analysis for rocket engine cooling systems design

Francesco Nasuti Information

University

Position

___

Citations(all)

4106

Citations(since 2020)

2043

Cited By

2792

hIndex(all)

37

hIndex(since 2020)

26

i10Index(all)

106

i10Index(since 2020)

68

Email

University Profile Page

Google Scholar

Francesco Nasuti Skills & Research Interests

Aerospace Propulsion

Top articles of Francesco Nasuti

Low-order modeling approach for the prediction of transverse combustion instabilities in multi-injector engines

CEAS Space Journal

2024/3/11

Francesco Nasuti
Francesco Nasuti

H-Index: 22

Design and Evaluation of Aerospike Nozzles for an Upper-Stage Application

Journal of Spacecraft and Rockets

2024/3

Francesco Nasuti
Francesco Nasuti

H-Index: 22

Daniele Bianchi
Daniele Bianchi

H-Index: 23

Family of Skeletal Reaction Mechanisms for Methane–Oxygen Combustion in Rocket Propulsion

Journal of Propulsion and Power

2024/1

Radiative Wall Heat Transfer Evaluation in Hybrid Rocket Thrust Chambers

2024

Modeling and Analysis of Film Cooling in Oxygen-Kerosene Rocket Thrust Chambers

2024

Low-Order Modeling of Combustion Instability: A Comprehensive Analysis of the BKD Test Case

2024

Marco Grossi
Marco Grossi

H-Index: 14

Francesco Nasuti
Francesco Nasuti

H-Index: 22

Transient Analysis of Liquid Rocket Engine Chilldown and Startup by Conjugate Heat Transfer Approach

2024

Francesco Nasuti
Francesco Nasuti

H-Index: 22

Conjugate heat transfer applied to transitory analysis for rocket engine cooling systems design

Aeronautics and Astronautics: AIDAA XXVII International Congress

2023/12/15

Francesco Nasuti
Francesco Nasuti

H-Index: 22

Direct numerical simulation of turbulent flow in pipes with realistic large roughness at the wall

Computers & Fluids

2015/2/15

Numerical Simulations of Fuel Shape Change in Paraffin–Oxygen Hybrid Rocket Engines

Journal of Propulsion and Power

2023/11

Numerical and experimental analysis of fuel regression rate in a lab-scale hybrid rocket engine with swirl injection

Aerospace Science and Technology

2023/9/1

Driving Mechanisms in Low-Order Modeling of Longitudinal Combustion Instability

Journal of Propulsion and Power

2023/9

Francesco Nasuti
Francesco Nasuti

H-Index: 22

A design strategy for water-based noise suppression systems in liquid rocket engines firing tests

CEAS Space Journal

2023/7

Numerical Simulations of Fuel Shape Change and Swirling Flows in Paraffin/Oxygen Hybrid Rocket Engines

Aerotecnica Missili & Spazio

2023/3

Study, development, implementation and testing of a water resistojet propulsion system for CubeSats

2023

Mario Tindaro Migliorino
Mario Tindaro Migliorino

H-Index: 4

Francesco Nasuti
Francesco Nasuti

H-Index: 22

Simplified Numerical Modeling of Film Cooling and Mixture Ratio Bias in Liquid Rocket Thrust Chambers

2023

Convective and Radiative Wall Heat Transfer Evaluation in Film-Cooled Liquid Rocket Thrust Chambers

2023

T (H) RUST: applied research activities on liquid rocket propulsion at Sapienza University of Rome

2023

Modeling of swirl injection effects in a H2O2-HDPE hybrid rocket

2023

Sensitivity Study on a Low Order Model for the Analysis of Transverse Combustion Instability

2023

Francesco Nasuti
Francesco Nasuti

H-Index: 22

See List of Professors in Francesco Nasuti University(Sapienza Università di Roma)

Co-Authors

academic-engine