A description of models and boundary conditions required for coupling radiation and ablation physics to a hypersonic flow simulation is provided. Chemical equilibrium routines for varying elemental mass fraction are required in the flow solver to integrate with the equilibrium chemistry assumption employed in the ablation models. The capability also enables an equilibrium catalytic wall boundary condition in the non-ablating case. The paper focuses on numerical implementation issues using FIRE II, Mars return, and Apollo 4 applications to provide context for discussion. Variable relaxation factors applied to the Jacobian elements of partial equilibrium relations required for convergence are defined. Challenges of strong radiation coupling i...
Cette thèse est centrée sur le couplage entre les phénomènes d’écoulement, d’ablation et de rayonnem...
To study the atmospheric reentry phase of a space vehicle, it is necessary tounderstand correctly th...
The present understanding of shock-layer radiation in the low density regime, as appropriate to hype...
A seven-species hypersonic flow solver that independently tracks vibrational energies of diatomic sp...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77076/1/AIAA-2009-3597-202.pd
During atmospheric entry, a spacecraft's aeroshell uses a thermal protection system (TPS) to withsta...
During the atmospheric entry of a blunt body, a bow shock wave is generated on the nose of the vehic...
We present a parallel solver for performing full-trajectory simulations of hypersonic ablating bodie...
A one-dimensional material response implicit solver with surface ablation and pyrolysis is strongly ...
© 2016 Chinese Society of Aeronautics and Astronautics. Ablation flows around entry bodies are at hi...
We study the gas-surface interaction of dissociated air in a high enthalpy flow. A framework that pr...
The mathematical and numerical formulation employed in the development of a new multi-dimensional Co...
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140702/1/1.A32847.pd
Hypersonic vehicles are subjected to high heat loads throughout their flight trajectories, and as a ...
This thesis focuses on the coupling between flow, ablation, and radiation phenomena encountered in t...
Cette thèse est centrée sur le couplage entre les phénomènes d’écoulement, d’ablation et de rayonnem...
To study the atmospheric reentry phase of a space vehicle, it is necessary tounderstand correctly th...
The present understanding of shock-layer radiation in the low density regime, as appropriate to hype...
A seven-species hypersonic flow solver that independently tracks vibrational energies of diatomic sp...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77076/1/AIAA-2009-3597-202.pd
During atmospheric entry, a spacecraft's aeroshell uses a thermal protection system (TPS) to withsta...
During the atmospheric entry of a blunt body, a bow shock wave is generated on the nose of the vehic...
We present a parallel solver for performing full-trajectory simulations of hypersonic ablating bodie...
A one-dimensional material response implicit solver with surface ablation and pyrolysis is strongly ...
© 2016 Chinese Society of Aeronautics and Astronautics. Ablation flows around entry bodies are at hi...
We study the gas-surface interaction of dissociated air in a high enthalpy flow. A framework that pr...
The mathematical and numerical formulation employed in the development of a new multi-dimensional Co...
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140702/1/1.A32847.pd
Hypersonic vehicles are subjected to high heat loads throughout their flight trajectories, and as a ...
This thesis focuses on the coupling between flow, ablation, and radiation phenomena encountered in t...
Cette thèse est centrée sur le couplage entre les phénomènes d’écoulement, d’ablation et de rayonnem...
To study the atmospheric reentry phase of a space vehicle, it is necessary tounderstand correctly th...
The present understanding of shock-layer radiation in the low density regime, as appropriate to hype...