Zobrazeno 1 - 10
of 36
pro vyhledávání: '"Cutrone, Luigi"'
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2022, Vol. 94, Issue 9, pp. 1499-1507.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-01-2022-0024
This paper provides an improved flamelet/progress variable (FPV) model for the simulation of turbulent combustion, employing the statistically most likely distribution (SMLD) approach for the joint probability density function (PDF) of the mixture fr
Externí odkaz:
http://arxiv.org/abs/1504.04957
Autor:
French, Ainslie, Cutrone, Luigi, Schettino, Antonio, Marini, Marco, Battista, Francesco, Natale, Pasquale
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2020, Vol. 92, Issue 9, pp. 1339-1344.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-01-2020-0006
This paper provides an extension of the standard flamelet progress variable (FPV) approach for turbulent combustion, applying the statistically most likely distribution (SMLD) framework to the joint PDF of the mixture fraction, Z, and the progress va
Externí odkaz:
http://arxiv.org/abs/1306.4863
Flamelet Progress Variable (FPV) combustion models allow the evaluation of all thermo chemical quantities in a reacting flow by computing only the mixture fraction Z and a progress variable C. When using such a method to predict a turbulent combustio
Externí odkaz:
http://arxiv.org/abs/1305.5893
Autor:
Bonelli, Francesco, Tuttafesta, Michele, Colonna, Gianpiero, Cutrone, Luigi, Pascazio, Giuseppe
Publikováno v:
In Computer Physics Communications October 2017 219:178-195
Autor:
Bonelli, Francesco, Tuttafesta, Michele, Colonna, Gianpiero, Cutrone, Luigi, Pascazio, Giuseppe
Publikováno v:
In Energy Procedia September 2017 126:99-106
Publikováno v:
In Acta Astronautica July 2017 136:148-158
Autor:
Cutrone, Luigi, Schettino, Antonio
Publikováno v:
Aerotecnica Missili & Spazio: Journal of Aerospace Science, Technologies & Systems; 20240101, Issue: Preprints p1-10, 10p
Autor:
French Ainslie D., Cutrone Luigi, Schettino Antonio, Marini Marco, Battista Francesco, Natale Pasquale
Publikováno v:
MATEC Web of Conferences, Vol 304, p 07007 (2019)
This study details the reactive flow simulations of a LOX/CH4 Multi-element rocket engine. The work has been conducted within the framework of the HYPROB-BREAD project whose main objective is the design, manufacture and testing of a LOX/LCH4 regenera
Externí odkaz:
https://doaj.org/article/b0634dbc18e944cabb2277c1a45e46bd