The present study focuses on the simulation of the aero-thermal interaction between the flow field surrounding a reentry vehicle and its thermal protection system (TPS). An interface tool has been developed to couple computational fluid-dynamics (CFD) results and thermo-structural simulations in order to evaluate the actual thermal loads acting on the structure along the re-entry trajectory. In order to show the efficiency of the developed tool, this technique has been applied to a meaningful two-dimensional test case, using MSC-Nastran as thermo-structural code. It is remarkable that, even though the presented model is two-dimensional, the above interface procedure has been developed to be applied to both 2D and 3D cases.
Thermal fluid-structure interaction on re-entry vehicle TPS / Borreca, S.; Tumino, G.; Gaudenzi, Paolo. - (2005), pp. 1218-1222. (Intervento presentato al convegno 3rd M.I.T. Conference on Computational Fluid and Solid Mechanics tenutosi a Boston, MA).
Thermal fluid-structure interaction on re-entry vehicle TPS
GAUDENZI, Paolo
2005
Abstract
The present study focuses on the simulation of the aero-thermal interaction between the flow field surrounding a reentry vehicle and its thermal protection system (TPS). An interface tool has been developed to couple computational fluid-dynamics (CFD) results and thermo-structural simulations in order to evaluate the actual thermal loads acting on the structure along the re-entry trajectory. In order to show the efficiency of the developed tool, this technique has been applied to a meaningful two-dimensional test case, using MSC-Nastran as thermo-structural code. It is remarkable that, even though the presented model is two-dimensional, the above interface procedure has been developed to be applied to both 2D and 3D cases.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
