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Tag Archives: High Enthalpy Shock Tunnel

Cavity-based Combustion Characteristics of a Mach 10 Scramjet

1.Events, HiSST 2024, Propulsion Systems and ComponentsBy Beata Wierzbińska-PrusMay 13, 2024

Hongbo LU, Hengyi WU, Jian LIN, Ruiting WANG, Feng JI, Xing CHEN

DOI Number: N/A

Conference number: HiSST-2024-091

Vibrational Non-equilibrium Effects in Compressed and Expanding Hypersonic High Enthalpy Flow

1.Events, High-Speed Aerodynamics and Aerothermodynamics, HiSST 2024By Beata Wierzbińska-PrusMay 10, 2024

Jan MARTINEZ SCHRAMM, Georgii OBLAPENKO

DOI Number: https://doi.org/10.82241/ceas-hisst-2024-079

Conference number: HiSST-2024-079

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