AbstractBoundary layers at a zero pressure gradient in chemical non-equilibrium are considered for a five-species model of air in a total enthalpy range of 5 - 17MJ/kg. Comparisons with boundary layers in binary mixtures of oxygen reveal that the growth rates of the second mode are lower in the case of air. This result can be attributed to the lower wall temperatures in binary mixtures of oxygen due to dissociation, with the lower wall temperatures having a destabilizing effect on the second mode similar to the case of boundary layers in calorically perfect gases
The influence of high-enthalpy effects on hypersonic turbulent boundary layers is investigated by me...
This paper presents a computational study of real-gas effects on the mean flow and temporal stabilit...
Prediction and control of boundary layer transition from laminar to turbulent is important to many f...
AbstractBoundary layers at a zero pressure gradient in chemical non-equilibrium are considered for a...
A hypersonic, spatially evolving turbulent boundary layer at Mach 12.48 with a cooled wall is analys...
More than 50 shots with air and 35 shots with carbon dioxide were carried out in the T5 shock tunnel...
Laminar to turbulent transition on a smooth 5-degree half angle cone at zero angle of attack is inve...
Binary scaling is a similitude law that facilitates the study of hypersonic flows around blunt bodie...
A Mach-10 hypersonic boundary layer of air overriding a cold, isothermal, non-catalytic flat wall, a...
The influence of high levels of wall cooling on the stability of hypervelocity boundary layers is in...
High-temperature effects arising in hypersonic flights have a major impact on aerodynamic performanc...
Analytical solutions are presented for a family of highly nonequilibrium (nearly frozen) boundary la...
A hypersonic laminar flow over double wedges with a fixed forward angle of 15 and varied aft angles ...
The present paper provides a comprehensive comparative analysis of thermochemistry models of various...
Understanding non-equilibrium effects of hypersonic turbulent boundary layers is essential in order ...
The influence of high-enthalpy effects on hypersonic turbulent boundary layers is investigated by me...
This paper presents a computational study of real-gas effects on the mean flow and temporal stabilit...
Prediction and control of boundary layer transition from laminar to turbulent is important to many f...
AbstractBoundary layers at a zero pressure gradient in chemical non-equilibrium are considered for a...
A hypersonic, spatially evolving turbulent boundary layer at Mach 12.48 with a cooled wall is analys...
More than 50 shots with air and 35 shots with carbon dioxide were carried out in the T5 shock tunnel...
Laminar to turbulent transition on a smooth 5-degree half angle cone at zero angle of attack is inve...
Binary scaling is a similitude law that facilitates the study of hypersonic flows around blunt bodie...
A Mach-10 hypersonic boundary layer of air overriding a cold, isothermal, non-catalytic flat wall, a...
The influence of high levels of wall cooling on the stability of hypervelocity boundary layers is in...
High-temperature effects arising in hypersonic flights have a major impact on aerodynamic performanc...
Analytical solutions are presented for a family of highly nonequilibrium (nearly frozen) boundary la...
A hypersonic laminar flow over double wedges with a fixed forward angle of 15 and varied aft angles ...
The present paper provides a comprehensive comparative analysis of thermochemistry models of various...
Understanding non-equilibrium effects of hypersonic turbulent boundary layers is essential in order ...
The influence of high-enthalpy effects on hypersonic turbulent boundary layers is investigated by me...
This paper presents a computational study of real-gas effects on the mean flow and temporal stabilit...
Prediction and control of boundary layer transition from laminar to turbulent is important to many f...