Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97085/1/AIAA2012-2873.pd
During hypersonic atmospheric entry, spacecraft are exposed to enormous aerodynamic heat. To prevent...
During the atmospheric entry of a blunt body, a bow shock wave is generated on the nose of the vehic...
Carbon/carbon composites are usually used as a thermal protection material in the nose cap and leadi...
Hypersonic vehicles are subjected to high heat loads throughout their flight trajectories, and as a ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77076/1/AIAA-2009-3597-202.pd
Re-entry of a spacecraft occurs at hypersonic regime where flow field is extremely complex. High tem...
Re-entry of a spacecraft occurs at the hypersonic regime where the flow field is extremely complex: ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77158/1/AIAA-2009-670-901.pd
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140702/1/1.A32847.pd
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140434/1/6.2014-2124.pd
This study demonstrates that coupling of a material thermal response code and a flow solver with non...
The development of a numerical code capable of simulating the multidimensional thermal and structura...
A one-dimensional material response implicit solver with surface ablation and pyrolysis is strongly ...
Development of a solver in order to estimate the material response of charring ablative materials w...
The interaction between a chemically reactive boundary layer and an ablative material is one of the ...
During hypersonic atmospheric entry, spacecraft are exposed to enormous aerodynamic heat. To prevent...
During the atmospheric entry of a blunt body, a bow shock wave is generated on the nose of the vehic...
Carbon/carbon composites are usually used as a thermal protection material in the nose cap and leadi...
Hypersonic vehicles are subjected to high heat loads throughout their flight trajectories, and as a ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77076/1/AIAA-2009-3597-202.pd
Re-entry of a spacecraft occurs at hypersonic regime where flow field is extremely complex. High tem...
Re-entry of a spacecraft occurs at the hypersonic regime where the flow field is extremely complex: ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77158/1/AIAA-2009-670-901.pd
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140702/1/1.A32847.pd
Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140434/1/6.2014-2124.pd
This study demonstrates that coupling of a material thermal response code and a flow solver with non...
The development of a numerical code capable of simulating the multidimensional thermal and structura...
A one-dimensional material response implicit solver with surface ablation and pyrolysis is strongly ...
Development of a solver in order to estimate the material response of charring ablative materials w...
The interaction between a chemically reactive boundary layer and an ablative material is one of the ...
During hypersonic atmospheric entry, spacecraft are exposed to enormous aerodynamic heat. To prevent...
During the atmospheric entry of a blunt body, a bow shock wave is generated on the nose of the vehic...
Carbon/carbon composites are usually used as a thermal protection material in the nose cap and leadi...
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