The Nonequilibrium Ablation and Pyrolysis (NEQAP) code implements a one-dimensional ablation and pyrolysis model derived from first principles for Carbon-Phenolic Thermal Protection Systems. Traditionally, ablation models assume in-depth pyrolysis gases to be in chemical equilibrium as well as in thermal equilibrium with surrounding char material. The goal of NEQAP is to remove these assumptions in order to study the effects they have on current material response predictions including pyrolysis gas composition in-depth and their flux into the boundary layer. The pyrolysis gas densities in-depth are computed by solving species mass conservation equations for a homogeneously reacting ow through a porous medium with the velocities approximated...
The present thesis provides a description of historical and current modeling methods with recent dis...
In the late 1950s, the earliest models describing the thermal response of ablative materials were ba...
Future space exploration missions foresee high-speed entries into planetary atmospheres. These latte...
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...
We are interested in participating in the inter-code calibration and validation exercise in the Four...
As the part of an ongoing study on heat flux and ablation on hypersonic vehicles, a one dimensional ...
Charring ablators remain the premium choice for space exploration missions that involve atmospheric ...
Low-density carbon/phenolic is a class of ablative materials that is attractive for blunt body space...
When a spacecraft traveling at orbital speeds enters a planetary atmosphere, shock waves and frictio...
To predict the high temperature behavior of a carbon/phenolic charring ablator, a model of the therm...
The Fully Implicit Ablation and Thermal Response code, FIAT, simulates pyrolysis and ablation of the...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76855/1/AIAA-2008-3805-224.pd
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...
The present thesis provides a description of historical and current modeling methods with recent dis...
In the late 1950s, the earliest models describing the thermal response of ablative materials were ba...
Future space exploration missions foresee high-speed entries into planetary atmospheres. These latte...
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...
We are interested in participating in the inter-code calibration and validation exercise in the Four...
As the part of an ongoing study on heat flux and ablation on hypersonic vehicles, a one dimensional ...
Charring ablators remain the premium choice for space exploration missions that involve atmospheric ...
Low-density carbon/phenolic is a class of ablative materials that is attractive for blunt body space...
When a spacecraft traveling at orbital speeds enters a planetary atmosphere, shock waves and frictio...
To predict the high temperature behavior of a carbon/phenolic charring ablator, a model of the therm...
The Fully Implicit Ablation and Thermal Response code, FIAT, simulates pyrolysis and ablation of the...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76855/1/AIAA-2008-3805-224.pd
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...
The present thesis provides a description of historical and current modeling methods with recent dis...
In the late 1950s, the earliest models describing the thermal response of ablative materials were ba...
Future space exploration missions foresee high-speed entries into planetary atmospheres. These latte...