Add to ORKGChemical and chemical radiative effects on base flow field of multiple nozzled launch vehicles of Saturn launch vehicle typ
Experimental study of effect of finite homogeneous reaction rates on heat transfer in turbulent tube...
Free molecular heat transfer and mass flux at vehicle surface during ionospheric entr
As part of a continuing study of the environmental effects of solid rocket motor (SRM) operations in...
A mathematical model of the aerothermochemical environment along the stagnation line of a planetary ...
Theoretical prediction of state of gas in flow field surrounding Apollo type vehicle in reentry at h...
Shear layer mixing, hydrocarbon oxidation, and carbon cloud radiation models for liquid rocket engin...
Flow field comparisons of Saturn S- II stage and spiked hemisphere configuration with emphasis on r...
A computational method was developed for the fully-coupled solution of nongray, radiating gas flows ...
Measurement of absorptivity and fine structure parameters of water vapor for use in evaluating radia...
An axisymmetric single engine Computational Fluid Dynamics calculation of the Saturn V/S 1-C vehicle...
Radiative and convective heat transfer about two blunt bodies traveling at hypersonic speeds at zero...
The radiation intensities are determined in the base region of the space shuttle due to solid partic...
This report includes copies of relevant publications, including conference proceedings, resulting fr...
Work performed during the first six months of the project duration for NASA Grant (NAG-1-861) is rep...
Prediction of Saturn V vehicle and launch complex force and heat load environments due to rocket jet...
Experimental study of effect of finite homogeneous reaction rates on heat transfer in turbulent tube...
Free molecular heat transfer and mass flux at vehicle surface during ionospheric entr
As part of a continuing study of the environmental effects of solid rocket motor (SRM) operations in...
A mathematical model of the aerothermochemical environment along the stagnation line of a planetary ...
Theoretical prediction of state of gas in flow field surrounding Apollo type vehicle in reentry at h...
Shear layer mixing, hydrocarbon oxidation, and carbon cloud radiation models for liquid rocket engin...
Flow field comparisons of Saturn S- II stage and spiked hemisphere configuration with emphasis on r...
A computational method was developed for the fully-coupled solution of nongray, radiating gas flows ...
Measurement of absorptivity and fine structure parameters of water vapor for use in evaluating radia...
An axisymmetric single engine Computational Fluid Dynamics calculation of the Saturn V/S 1-C vehicle...
Radiative and convective heat transfer about two blunt bodies traveling at hypersonic speeds at zero...
The radiation intensities are determined in the base region of the space shuttle due to solid partic...
This report includes copies of relevant publications, including conference proceedings, resulting fr...
Work performed during the first six months of the project duration for NASA Grant (NAG-1-861) is rep...
Prediction of Saturn V vehicle and launch complex force and heat load environments due to rocket jet...
Experimental study of effect of finite homogeneous reaction rates on heat transfer in turbulent tube...
Free molecular heat transfer and mass flux at vehicle surface during ionospheric entr
As part of a continuing study of the environmental effects of solid rocket motor (SRM) operations in...