As the part of an ongoing study on heat flux and ablation on hypersonic vehicles, a one dimensional material response implicit solver with solid ablation and pyrolysis has been developed at the University of Michigan. This code, named MOPAR, uses the Control Volume Finite-Element Method (CVFEM) to model surface ablation with wall recession, as well as inner decomposition and pyrolysis gas behavior. The code solves the solid and gas phase mass conservation equations, the total energy (solid and gas) conservation equation as well as the momentum conservation equation. The latter is pore-averaged to the Forchheimer Law. In addition, MOPAR also takes into account variable coordinate systems (cylindrical and spherical), and allows ablation on bo...
The development of a methodology and computational framework for performing conjugate analyses of tr...
Hypersonic vehicles are subjected to high heat loads throughout their flight trajectories, and as a ...
Using an ablative thermal/material response code, the importance of three-dimensionality for modelin...
We are interested in participating in the inter-code calibration and validation exercise in the Four...
Charring ablative thermal protection system (TPS) has been commonly used to prevent the payload of a...
In the frame of its activities NASA as defined a one dimensional test case for assessing the capabil...
The Nonequilibrium Ablation and Pyrolysis (NEQAP) code implements a one-dimensional ablation and pyr...
Low-density carbon/phenolic is a class of ablative materials that is attractive for blunt body space...
Future space exploration missions foresee high-speed entries into planetary atmospheres. These latte...
The Aerotherm CMA code and associated model are the basis for most present in-depth ablation and the...
This study demonstrates that coupling of a material thermal response code and a flow solver with non...
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
Charring ablators remain the premium choice for space exploration missions that involve atmospheric ...
In the late 1950s, the earliest models describing the thermal response of ablative materials were ba...
The development of a methodology and computational framework for performing conjugate analyses of tr...
Hypersonic vehicles are subjected to high heat loads throughout their flight trajectories, and as a ...
Using an ablative thermal/material response code, the importance of three-dimensionality for modelin...
We are interested in participating in the inter-code calibration and validation exercise in the Four...
Charring ablative thermal protection system (TPS) has been commonly used to prevent the payload of a...
In the frame of its activities NASA as defined a one dimensional test case for assessing the capabil...
The Nonequilibrium Ablation and Pyrolysis (NEQAP) code implements a one-dimensional ablation and pyr...
Low-density carbon/phenolic is a class of ablative materials that is attractive for blunt body space...
Future space exploration missions foresee high-speed entries into planetary atmospheres. These latte...
The Aerotherm CMA code and associated model are the basis for most present in-depth ablation and the...
This study demonstrates that coupling of a material thermal response code and a flow solver with non...
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
Charring ablators remain the premium choice for space exploration missions that involve atmospheric ...
In the late 1950s, the earliest models describing the thermal response of ablative materials were ba...
The development of a methodology and computational framework for performing conjugate analyses of tr...
Hypersonic vehicles are subjected to high heat loads throughout their flight trajectories, and as a ...
Using an ablative thermal/material response code, the importance of three-dimensionality for modelin...