Vydavatel National Aeronautics and Space Administration
Datum vydání před téměř 10 roky
Shrnutí
Popis
<p>A predictive tool with tight coupling of the fluid and thermal physics will give insights into the conservatism of the uncoupled design process and could lead to margin reduction and consequently reduced heat shield mass. This project seeks to couple the CHarring Ablator Response (CHAR) code and the Fully Implicit Navier-Stokes (FIN-S) code with finite-rate models governing the gas-surface interactions and surface mass loss.&nbsp; Loose coupling has already been demonstrated between the codes for non-ablating materials, which helped identify and solve potential computer science and physical modeling issues. Additionally, the development team has already shown an ability to implement a multi-physics simulation framework as they have recently coupled thermal and structural physics modules within the CHAR code. The bulk of the work focuses on modeling the energy flux terms at the gas-surface interface. The current design approach requires gross assumptions or even neglecting terms in either the CFD or AMR analyses.</p><p>Progress to date has included the integration of the software components into one executable that facilitates information exchange between the fluid and ablation physics.&nbsp; The software has been demonstrated on both two and three dimensional ablation problems.&nbsp; On going efforts include verification and validation of the new multi-physics software tool.</p>