Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97122/1/AIAA2012-534.pd
With a growing demand for cheap access to space and high-speed flight, hypersonic research is experi...
The rate of nitridation reaction at graphite surface is evaluated in an inductively coupled plasma h...
The re-entry vehicle posseses enough kinetic energy that it becomes hypersonic while passing through...
The high temperatures on a hypersonic vehicle surface caused by heat loads encountered during (re-)e...
The high temperatures on a hypersonic vehicle surface caused by heat loads encountered during (re-)e...
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140701/1/1.T4530.pd
The aerothermal heating of a Thermal Protection System (TPS) is significantly affected by the physic...
The high temperatures on a hypersonic vehicle surface caused by heat loads encountered during entry ...
The high-enthalpy flow generated by hypersonic vehicles traveling within the Earth\u27s atmosphere i...
Nitrogen injection effects on boundary layer of graphite surface in high-temperature dissociated air...
In the design of a thermal protection system for atmospheric entry, aerothermal heating presents a m...
Accurate knowledge of heat transfer to materials in recombining plasmas is needed to improve heat sh...
A model for heterogeneous catalysis for Copper, Nickel, and Platinum has been devised. The model sim...
During the (re-)entry phase of a space vehicle, the gas flow in the shock layer can be in a state o...
The catalytic efficiency (atom recombination coefficients) for advanced ceramic thermal protection s...
With a growing demand for cheap access to space and high-speed flight, hypersonic research is experi...
The rate of nitridation reaction at graphite surface is evaluated in an inductively coupled plasma h...
The re-entry vehicle posseses enough kinetic energy that it becomes hypersonic while passing through...
The high temperatures on a hypersonic vehicle surface caused by heat loads encountered during (re-)e...
The high temperatures on a hypersonic vehicle surface caused by heat loads encountered during (re-)e...
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140701/1/1.T4530.pd
The aerothermal heating of a Thermal Protection System (TPS) is significantly affected by the physic...
The high temperatures on a hypersonic vehicle surface caused by heat loads encountered during entry ...
The high-enthalpy flow generated by hypersonic vehicles traveling within the Earth\u27s atmosphere i...
Nitrogen injection effects on boundary layer of graphite surface in high-temperature dissociated air...
In the design of a thermal protection system for atmospheric entry, aerothermal heating presents a m...
Accurate knowledge of heat transfer to materials in recombining plasmas is needed to improve heat sh...
A model for heterogeneous catalysis for Copper, Nickel, and Platinum has been devised. The model sim...
During the (re-)entry phase of a space vehicle, the gas flow in the shock layer can be in a state o...
The catalytic efficiency (atom recombination coefficients) for advanced ceramic thermal protection s...
With a growing demand for cheap access to space and high-speed flight, hypersonic research is experi...
The rate of nitridation reaction at graphite surface is evaluated in an inductively coupled plasma h...
The re-entry vehicle posseses enough kinetic energy that it becomes hypersonic while passing through...
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