A nonequilibrium radiative heating prediction method has been used to evaluate several energy exchange models used in nonequilibrium computational fluid dynamics methods. The radiative heating measurements from the FIRE II flight experiment supply an experimental benchmark against which different formulations for these exchange models can be judged. The models which predict the lowest radiative heating are found to give the best agreement with the flight data. Examination of the spectral distribution of radiation indicates that despite close agreement of the total radiation, many of the models examined predict excessive molecular radiation. It is suggested that a study of the nonequilibrium chemical kinetics may lead to a correction for thi...
The numerical simulation of hypersonic ow in thermochemical nonequilibrium over the forebody of the ...
An accurate analysis of nonequilibrium air plasma flows is performed by using a one-dimensional shoc...
The objective of this study was to investigate the uncertainty in shock layer radiative heat predict...
A radiative heat transfer code, based on the Discrete Transfer method, is used in combination with ...
A method for predicting radiation adsorption and emission coefficients in thermochemical nonequilibr...
Accurate prediction of the aerothermal environment is of great significance to space exploration and...
This final report will attempt to concisely summarize the activities and accomplishments associated ...
A method for predicting radiative heating and coupling effects in nonequilibrium flow-fields has bee...
Approximations applicable to the radiating, reacting, and conducting stagnation region of a hypervel...
Measurements of stagnation heat transfer rates to the surface of a small model of an aerobraking veh...
The aerothermal environment is examined for two vehicle forebodies near the peak heating points of l...
An accurate analysis of nonequilibrium air plasma flows is performed by using a one-dimensional shoc...
During atmospheric entry, a spacecraft's aeroshell uses a thermal protection system (TPS) to withsta...
An accurate analysis of nonequilibrium air plasma flows is performed by using a one-dimensional shoc...
An accurate analysis of nonequilibrium air plasma flows is performed by using a one-dimensional shoc...
The numerical simulation of hypersonic ow in thermochemical nonequilibrium over the forebody of the ...
An accurate analysis of nonequilibrium air plasma flows is performed by using a one-dimensional shoc...
The objective of this study was to investigate the uncertainty in shock layer radiative heat predict...
A radiative heat transfer code, based on the Discrete Transfer method, is used in combination with ...
A method for predicting radiation adsorption and emission coefficients in thermochemical nonequilibr...
Accurate prediction of the aerothermal environment is of great significance to space exploration and...
This final report will attempt to concisely summarize the activities and accomplishments associated ...
A method for predicting radiative heating and coupling effects in nonequilibrium flow-fields has bee...
Approximations applicable to the radiating, reacting, and conducting stagnation region of a hypervel...
Measurements of stagnation heat transfer rates to the surface of a small model of an aerobraking veh...
The aerothermal environment is examined for two vehicle forebodies near the peak heating points of l...
An accurate analysis of nonequilibrium air plasma flows is performed by using a one-dimensional shoc...
During atmospheric entry, a spacecraft's aeroshell uses a thermal protection system (TPS) to withsta...
An accurate analysis of nonequilibrium air plasma flows is performed by using a one-dimensional shoc...
An accurate analysis of nonequilibrium air plasma flows is performed by using a one-dimensional shoc...
The numerical simulation of hypersonic ow in thermochemical nonequilibrium over the forebody of the ...
An accurate analysis of nonequilibrium air plasma flows is performed by using a one-dimensional shoc...
The objective of this study was to investigate the uncertainty in shock layer radiative heat predict...