Experimental measurements on Tekna’’PlasmaSonic’’ High EnthalpyGround Testing Facilities using 350 kW ICPT plasma torch to reproduce re-entry conditions of space vehicles
Y. Lakaf, S. Xue
DOI Number XXX-YYY-ZZZ
Conference Number HiSST-2022-0404
Coupled fluid / thermal computation of ablating graphite material usingnonequilibrium chemistry during atmospheric entry
Vivien Loridan, Simon Peluchon, Jean Claudel
DOI Number XXX-YYY-ZZZ
Conference Number HiSST-2022-04
Experimental Study of Shock/Shock Interferences in a Hypersonic Mach20.2 Rarefied Flow
Vincente Cardona, Viviana Lago
DOI Number XXX-YYY-ZZZ
Conference Number HiSST-2022-402
Re-entry Analyses of Space Debris with Surface Oxidation, Ablation, andBy-products Generation
Seong-Hyeon Park, Javier Navarro Laboulais, Pénélope Leyland, Stefano Mischler
DOI Number XXX-YYY-ZZZ
Conference Number HiSST-2022-0401
Simulating Hypersonic Fluid Structural Interaction of an InclinedCantilever Panel Using the Conservation Element Solution Element Method
L. Pollock, G. Wild
DOI Number XXX-YYY-ZZZ
Conference Number HiSST-2022-400
Temporary Fiber Bragg Grating Sensors for Static and Dynamic Strain Measurements in Hypersonic Wind Tunnels
L. Pollock, G. Wild
DOI Number XXX-YYY-ZZZ
Conference Number HiSST-2022-399