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Technische Universität Berlin (TUB)
Experimental investigations of low total pressure loss injectors on wave stabilization and performance
Technische Universiteit Eindhoven (TUE)
Fundamental study on the propagation mechanism of H2-air detonation under RDC-relevant conditions
Deutsches Zentrum für Luft- und Raumfahrt (DLR)
Experimental investigation of fuel-rich RDCs for gas generator applications
Office National d'Etudes et de Recherches Aérospatiales (ONERA)
Numerical study of injection and mixing in an airbreathing RDC
Ecole Nationale Supérieure de Mécanique et d’Aérotechnique (ENSMA)
Unsteady wall heat flux measurements under detonation conditions
Interaction of the combustor and transition duct on RDC performance and unsteadiness
Centre Européen de Recherche et de Formation Avancée en Calcul Scientifique (CERFACS)
High fidelity LES of RDE combustion chamber coupled with ejector (RDE design optimization)
Safran SA (SAFRAN)
Theoretical and numerical ejector modelling for subsonic turbine integration in RDC
Universita degli Studi di Firenze (UNIFI)
Numerical and experimental investigations of realistic cooling schemes in RDC
Politecnico di Torino (POLITO)
Design optimization of high-performance integrated transition duct and vanes for RDCs
The von Karman Institute for Fluid Dynamics (VKI)
Experimental testing of a subsonic turbine cascade under pulsating inflow conditions
Kungliga Tekniska Högskolan (KTH)
Numerical investigation of a supersonic axial turbine cascade for cooling and efficiency enhancement under RDC conditions
Politecnico di Milano (POLIMI)
Design and experimental testing of a supersonic turbine cascade under unsteady conditions
Radial RDC test rig coupled with a radial supersonic turbine
Università degli Studi di Genova (UNIGE)
Thermo-economic optimization and hybridization strategies
