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.
Strongly Coupled Computation of Material Response and Nonequilibrium Flow for Hypersonic Ablation [link]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},
}

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