The Aerotherm CMA code and associated model are the basis for most present in-depth ablation and thermal response analysis methods. In this poster, we re-examine the basic governing equations and recast them in conservation-law form, which is more amenable for use with current computational methods. The basic approximations for the CMA model are retained, and the results are compared to the solution of the CMA form of the equations for the TACOT test problem. The use of a Darcy Law for the pyrolysis gas flow and the assumptions associated with the pyrolysis gas state are also investigated
Future space exploration missions foresee high-speed entries into planetary atmospheres. These latte...
The development of a methodology and computational framework for performing conjugate analyses of tr...
The differential equations governing the transient response of a one-dimensional ablative thermal pr...
As the part of an ongoing study on heat flux and ablation on hypersonic vehicles, a one dimensional ...
In the frame of its activities NASA as defined a one dimensional test case for assessing the capabil...
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...
The Nonequilibrium Ablation and Pyrolysis (NEQAP) code implements a one-dimensional ablation and pyr...
In the late 1950s, the earliest models describing the thermal response of ablative materials were ba...
The material thermal response code CMA was used as part of a NASA/Air Force/Sandia code comparison e...
Low-density carbon/phenolic is a class of ablative materials that is attractive for blunt body space...
The Fully Implicit Ablation and Thermal Response code, FIAT, simulates pyrolysis and ablation of the...
The TACOT testcase will be computed using FGE\u27s ablation code FABL. Results will be presented for...
The workshop organizers defined a relatively simple case for this initial code intercalibration exer...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76855/1/AIAA-2008-3805-224.pd
Future space exploration missions foresee high-speed entries into planetary atmospheres. These latte...
The development of a methodology and computational framework for performing conjugate analyses of tr...
The differential equations governing the transient response of a one-dimensional ablative thermal pr...
As the part of an ongoing study on heat flux and ablation on hypersonic vehicles, a one dimensional ...
In the frame of its activities NASA as defined a one dimensional test case for assessing the capabil...
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...
The Nonequilibrium Ablation and Pyrolysis (NEQAP) code implements a one-dimensional ablation and pyr...
In the late 1950s, the earliest models describing the thermal response of ablative materials were ba...
The material thermal response code CMA was used as part of a NASA/Air Force/Sandia code comparison e...
Low-density carbon/phenolic is a class of ablative materials that is attractive for blunt body space...
The Fully Implicit Ablation and Thermal Response code, FIAT, simulates pyrolysis and ablation of the...
The TACOT testcase will be computed using FGE\u27s ablation code FABL. Results will be presented for...
The workshop organizers defined a relatively simple case for this initial code intercalibration exer...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76855/1/AIAA-2008-3805-224.pd
Future space exploration missions foresee high-speed entries into planetary atmospheres. These latte...
The development of a methodology and computational framework for performing conjugate analyses of tr...
The differential equations governing the transient response of a one-dimensional ablative thermal pr...