1–20 von 148 Ergebnissen
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    Ablative Material Behavior in Oxygen/Methane Thruster Environment

    Turchi, Alessandro / Bianchi, Daniele / Nasuti, Francesco et al. | AIAA | 2012

    A Computational Tool for the Design of Hybrid Rockets

    Freier Zugriff
    Zolla, Paolo Maria / Migliorino, Mario Tindaro / Bianchi, Daniele et al. | Springer Verlag | 2021

    Aerothermodynamic Analysis of Reentry Flows with Coupled Ablation

    Bianchi, Daniele / Nasuti, Francesco / Onofri, Marcello | AIAA | 2011

    A Hybrid Real/Ideal Gas Mixture Model in the Framework of Low Order Modeling of Combustion Instability

    D'Alessandro, Simone / Zolla, Paolo Maria / Pizzarelli, Marco et al. | AIAA | 2021

    A HYBRID REAL/IDEAL GAS MIXTURE MODEL IN THE FRAMEWORK OF LOW ORDER MODELING OF COMBUSTION INSTABILITY

    D'Alessandro, Simone / Zolla, Paolo Maria / Pizzarelli, Marco et al. | TIBKAT | 2021

    A low order modeling approach to transverse combustion instability

    D'Alessandro, Simone / Favini, Bernardo / Nasuti, Francesco | AIAA | 2019

    A LOW ORDER MODELING APPROACH TO TRANSVERSE COMBUSTION INSTABILITY

    D'Alessandro, Simone / Favini, Bernardo / Nasuti, Francesco | TIBKAT | 2019

    A methodology to study the possible occurrence of chugging in liquid rocket engines during transient start-up

    Leonardi, Marco / Nasuti, Francesco / Di Matteo, Francesco et al. | Elsevier | 2017

    A Multi-dimensional Approach for Low Order Modeling of Combustion Instability in a Rocket Combustor

    D'Alessandro, Simone / Frezzotti, Maria Luisa / Favini, Bernardo et al. | AIAA | 2018

    Analysis of Three-dimensional Flow Generated by a Linear Aerospike

    Geron, Marco / Paciorri, Renato / Nasuti, Francesco et al. | AIAA | 2005

    Analysis on the Effect of Channel Aspect Ratio on Rocket Thermal Behavior

    Pizzarelli, Marco / Nasuti, Francesco / Onofri, Marcello | AIAA | 2012

    Angle of attack guidance via robust approximate inversion

    Innocenti, Mario / Carnasciali, Gianluca / Nasuti, Francesco | AIAA | 1998

    A Numerical Approach for High-Temperature Flows over Ablating Surfaces

    Bianchi, Daniele / Nasuti, Francesco / Martelli, Emanuele et al. | AIAA | 2007

    A Numerical Model for Supercritical Flow in Rocket Engine Applications

    Pizzarelli, Marco / Paciorri, Renato / Nasuti, Francesco et al. | AIAA | 2007

    A numerical study of wake behavior in plug nozzles

    Nasuti, Francesco / Onofri, Marcello | AIAA | 2001

    A SENSITIVITY STUDY ON A CFD MODEL FOR PARAFFIN-BASED HYBRID ROCKETS

    Migliorino, Mario Tindaro / Bianchi, Daniele / Nasuti, Francesco | TIBKAT | 2020

    A Sensitivity Study on a CFD Model for Paraffin-based Hybrid Rockets

    Migliorino, Mario Tindaro / Bianchi, Daniele / Nasuti, Francesco | AIAA | 2020

    Assessment of a Conjugate Heat Transfer Model for Rocket Engine Cooling Channels Fed with Supercritical Methane

    Pizzarelli, Marco / Nasuti, Francesco / Votta, Raffaele et al. | AIAA | 2015

    Assessment of detached eddy simulation of a separated flow in a planar nozzle

    Martelli, Emanuele / Ciottoli, Pietro Paolo / Bernardini, Matteo et al. | AIAA | 2018