Models, which describe heat conduction within Thermal Protection System (TPS) materials and radiative exchange at the surface of space vehicles have been developed to supplement catalysis modelling at the sur-face with the aim of accurate prediction of the thermal loads during re-entry. These models have been de-veloped for the 3D Parallel-Multiblock (P-MB) URANUS code. Results and influence of the modelling are demonstrated on hand of the re-entry vehicle X-38 with real TPS coating.
Stationary coupling of 3D hypersonic nonequilibrium flows and TPS structure with URANUS
Stationäre Kopplung dreidimensionaler hypersonischer nicht-Gleichgewichtsströmungen mit TPS-Strukturen mit URANUS
AIAA Computational Fluid Dynamics Conference, 16 ; 1383-1398
2003
16 Seiten, 14 Bilder, 22 Quellen
Aufsatz (Konferenz)
Englisch
Stationary Coupling of Hypersonic Nonequilibrium Flows and Thermal-Protection-System Structure
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