Add to ORKGA one-dimensional material response implicit solver with surface ablation and pyrolysis is strongly coupled to LeMANS, a CFD code for the simulation of weakly ionized hypersonic flows in thermo-chemical non-equilibrium. Using blowing wall boundary conditions and a moving mesh algorithm, the results of a strongly coupled solution of a re-entry problem are presented, using the well defined case of the IRV-2 vehicle. Results are compared to other coupled codes and show good agreement with published numerical results
As the part of an ongoing study on heat flux and ablation on hypersonic vehicles, a one dimensional ...
During atmospheric entry, a spacecraft's aeroshell uses a thermal protection system (TPS) to withsta...
In this paper, we study the phenomena of thermo-chemical imbalance in a reactive mono-dimensional fl...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77076/1/AIAA-2009-3597-202.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77158/1/AIAA-2009-670-901.pd
The mathematical and numerical formulation employed in the development of a new multi-dimensional Co...
Hypersonic vehicles are subjected to high heat loads throughout their flight trajectories, and as a ...
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140702/1/1.A32847.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97085/1/AIAA2012-2873.pd
A description of models and boundary conditions required for coupling radiation and ablation physics...
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140434/1/6.2014-2124.pd
Numerical simulations of axisymmetric flows over reentry configurations at hypersonic conditions usi...
Re-entry of a spacecraft occurs at hypersonic regime where flow field is extremely complex. High tem...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76855/1/AIAA-2008-3805-224.pd
This dissertation concerns the development of a loosely coupled, finite element method for the numer...
As the part of an ongoing study on heat flux and ablation on hypersonic vehicles, a one dimensional ...
During atmospheric entry, a spacecraft's aeroshell uses a thermal protection system (TPS) to withsta...
In this paper, we study the phenomena of thermo-chemical imbalance in a reactive mono-dimensional fl...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77076/1/AIAA-2009-3597-202.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77158/1/AIAA-2009-670-901.pd
The mathematical and numerical formulation employed in the development of a new multi-dimensional Co...
Hypersonic vehicles are subjected to high heat loads throughout their flight trajectories, and as a ...
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140702/1/1.A32847.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97085/1/AIAA2012-2873.pd
A description of models and boundary conditions required for coupling radiation and ablation physics...
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140434/1/6.2014-2124.pd
Numerical simulations of axisymmetric flows over reentry configurations at hypersonic conditions usi...
Re-entry of a spacecraft occurs at hypersonic regime where flow field is extremely complex. High tem...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76855/1/AIAA-2008-3805-224.pd
This dissertation concerns the development of a loosely coupled, finite element method for the numer...
As the part of an ongoing study on heat flux and ablation on hypersonic vehicles, a one dimensional ...
During atmospheric entry, a spacecraft's aeroshell uses a thermal protection system (TPS) to withsta...
In this paper, we study the phenomena of thermo-chemical imbalance in a reactive mono-dimensional fl...