Nicole Viola

2 ta ish

Polytechnic University of Turin

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/2024.article.010229

2. Inflatable Heat Shields Solutions for Hypersonic Re-entry Applications: the European Commission EFESTO-2 Project

   GUIDOTTI, Giuseppe, TOSO, Federico, A. Princi +16

   MaqolaOAOchiq kirishGas Dynamics and Kinetic TheoryHAL (Le Centre pour la Communication Scientifique Directe)20240 iqtibos

   ABIABI:AkademIndex/2024.article.010235