Fabrizio Borgna

1 ta ish

Politecnico di Torino

1. Propulsive and Combustion Modelling of SABRE Engine in Rocket Mode to Support NOx Emissions Estimation in Conceptual Design

   Alessio Ricca, Valeria Borio, Roberta Fusaro +3

   MaqolaRocket and propulsion systems research20240 iqtibos

   ABIABI:AkademIndex/openalex/2024.article.010229