A procedure is developed for the prediction of radiation transport events in the context of the entry heating environment. The equivalent-width and exponential approximations are employed to reduce the computational requirements of the governing equations. Novel features are introduced in the use of an Elsasser band model to estimate line overlapping events and in the formulation of the wall reflection events. A matrix of calculations is presented to allow an assessment of the trade-offs between accuracy and computational efforts. It is concluded that the equivalent width model allows significant savings in computational effort with only modest penalties in accuracy. Consequently, the model should be viewed as an attractive candidate for us...
Convective and equilibrium radiation heat transfer prediction for Project Fire reentry vehicl
A JANNAF sponsored workshop was held to discuss the importance and role of radiative heat transfer i...
The effects of radiation on the performance of modern rocket propulsion systems operating at high pr...
Prediction method for calculating radiation transport in ablation product contaminated, hypersonic b...
The line-by-line accurate spectral radiation solver SPRADIAN was integrated with the multi-temperatu...
A method is presented for calculating nongrey radiative fluxes and intensities in a highly ionized, ...
Monte Carlo codes for IBM 7090 digital computer to calculate radiation heating in propellant tanks, ...
The methods are described which are used in predicting the thermal radiation received by space shutt...
A method for predicting radiation adsorption and emission coefficients in thermochemical nonequilibr...
A nonequilibrium, axisymmetric, Navier-Stokes flow solver with coupled radiation has been developed ...
The radiation models were compared on the basis of the approaches used for the transport calculation...
This paper presents measurements and simulations of non-equilibrium shock layer radiation relevant t...
Electron penetration calculational techniques are reviewed with regard to their suitability for shie...
A computational tool to simulate thermal radiation between surfaces is developed. The output is veri...
High-fidelity combustion simulations necessitate the accurate and efficient calculation of radiative...
Convective and equilibrium radiation heat transfer prediction for Project Fire reentry vehicl
A JANNAF sponsored workshop was held to discuss the importance and role of radiative heat transfer i...
The effects of radiation on the performance of modern rocket propulsion systems operating at high pr...
Prediction method for calculating radiation transport in ablation product contaminated, hypersonic b...
The line-by-line accurate spectral radiation solver SPRADIAN was integrated with the multi-temperatu...
A method is presented for calculating nongrey radiative fluxes and intensities in a highly ionized, ...
Monte Carlo codes for IBM 7090 digital computer to calculate radiation heating in propellant tanks, ...
The methods are described which are used in predicting the thermal radiation received by space shutt...
A method for predicting radiation adsorption and emission coefficients in thermochemical nonequilibr...
A nonequilibrium, axisymmetric, Navier-Stokes flow solver with coupled radiation has been developed ...
The radiation models were compared on the basis of the approaches used for the transport calculation...
This paper presents measurements and simulations of non-equilibrium shock layer radiation relevant t...
Electron penetration calculational techniques are reviewed with regard to their suitability for shie...
A computational tool to simulate thermal radiation between surfaces is developed. The output is veri...
High-fidelity combustion simulations necessitate the accurate and efficient calculation of radiative...
Convective and equilibrium radiation heat transfer prediction for Project Fire reentry vehicl
A JANNAF sponsored workshop was held to discuss the importance and role of radiative heat transfer i...
The effects of radiation on the performance of modern rocket propulsion systems operating at high pr...