Strongly Coupled Computation of Material Response and Nonequilibrium Flow for Hypersonic Ablation. Martin, A. & Boyd, I. D. Journal of Spacecraft and Rockets, 52(1):89–104, American Institute of Aeronautics and Astronautics, February, 2015.
Paper doi abstract bibtex 1 download The steps necessary to achieve the strong coupling between a flowfield solver and a material response solver are presented. This type of coupling is required to accurately capture the complex aerot...
@article{martin2015,
title = {Strongly {Coupled} {Computation} of {Material} {Response} and {Nonequilibrium} {Flow} for {Hypersonic} {Ablation}},
volume = {52},
url = {https://arc.aiaa.org/doi/abs/10.2514/1.A32847},
doi = {10.2514/1.A32847},
abstract = {The steps necessary to achieve the strong coupling between a flowfield solver and a material response solver are presented. This type of coupling is required to accurately capture the complex aerot...},
number = {1},
journal = {Journal of Spacecraft and Rockets},
publisher = {American Institute of Aeronautics and Astronautics},
author = {Martin, Alexandre and Boyd, Iain D.},
month = feb,
year = {2015},
keywords = {Arbitrary Lagrangian Eulerian, Boundary Layer, Courant Friedrichs Lewy, Freestream Mach Number, Heat Flux, Hypersonic Ablation, Hypersonic Aerothermodynamics, Nonequilibrium Flows, Pyrolysis, Stagnation Point},
pages = {89--104},
}
Downloads: 1
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