@article{
 title = {Strongly Coupled Computation of Material Response and Nonequilibrium Flow for Hypersonic Ablation},
 type = {article},
 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},
 volume = {52},
 websites = {https://arc.aiaa.org/doi/abs/10.2514/1.A32847},
 month = {2},
 publisher = {American Institute of Aeronautics and Astronautics},
 day = {19},
 id = {117cf66c-731b-3cbc-854b-6f7d72e3e6b8},
 created = {2021-10-03T20:54:08.942Z},
 accessed = {2021-10-03},
 file_attached = {true},
 profile_id = {6476e386-2170-33cc-8f65-4c12ee0052f0},
 group_id = {5a9f751c-3662-3c8e-b55d-a8b85890ce20},
 last_modified = {2021-10-03T20:54:10.159Z},
 read = {false},
 starred = {false},
 authored = {false},
 confirmed = {false},
 hidden = {false},
 citation_key = {martin:jsr:2015},
 private_publication = {false},
 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...},
 bibtype = {article},
 author = {Martin, Alexandre and Boyd, Iain D.},
 doi = {10.2514/1.A32847},
 journal = {Journal of Spacecraft and Rockets},
 number = {1}
}

{"_id":"nqnKMTmMQNexrvBPy","bibbaseid":"martin-boyd-stronglycoupledcomputationofmaterialresponseandnonequilibriumflowforhypersonicablation-2015","author_short":["Martin, A.","Boyd, I., D."],"bibdata":{"title":"Strongly Coupled Computation of Material Response and Nonequilibrium Flow for Hypersonic Ablation","type":"article","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","volume":"52","websites":"https://arc.aiaa.org/doi/abs/10.2514/1.A32847","month":"2","publisher":"American Institute of Aeronautics and Astronautics","day":"19","id":"117cf66c-731b-3cbc-854b-6f7d72e3e6b8","created":"2021-10-03T20:54:08.942Z","accessed":"2021-10-03","file_attached":"true","profile_id":"6476e386-2170-33cc-8f65-4c12ee0052f0","group_id":"5a9f751c-3662-3c8e-b55d-a8b85890ce20","last_modified":"2021-10-03T20:54:10.159Z","read":false,"starred":false,"authored":false,"confirmed":false,"hidden":false,"citation_key":"martin:jsr:2015","private_publication":false,"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...","bibtype":"article","author":"Martin, Alexandre and Boyd, Iain D.","doi":"10.2514/1.A32847","journal":"Journal of Spacecraft and Rockets","number":"1","bibtex":"@article{\n title = {Strongly Coupled Computation of Material Response and Nonequilibrium Flow for Hypersonic Ablation},\n type = {article},\n year = {2015},\n keywords = {Arbitrary Lagrangian Eulerian,Boundary Layer,Courant Friedrichs Lewy,Freestream Mach Number,Heat Flux,Hypersonic Ablation,Hypersonic Aerothermodynamics,Nonequilibrium Flows,Pyrolysis,Stagnation Point},\n pages = {89-104},\n volume = {52},\n websites = {https://arc.aiaa.org/doi/abs/10.2514/1.A32847},\n month = {2},\n publisher = {American Institute of Aeronautics and Astronautics},\n day = {19},\n id = {117cf66c-731b-3cbc-854b-6f7d72e3e6b8},\n created = {2021-10-03T20:54:08.942Z},\n accessed = {2021-10-03},\n file_attached = {true},\n profile_id = {6476e386-2170-33cc-8f65-4c12ee0052f0},\n group_id = {5a9f751c-3662-3c8e-b55d-a8b85890ce20},\n last_modified = {2021-10-03T20:54:10.159Z},\n read = {false},\n starred = {false},\n authored = {false},\n confirmed = {false},\n hidden = {false},\n citation_key = {martin:jsr:2015},\n private_publication = {false},\n 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...},\n bibtype = {article},\n author = {Martin, Alexandre and Boyd, Iain D.},\n doi = {10.2514/1.A32847},\n journal = {Journal of Spacecraft and Rockets},\n number = {1}\n}","author_short":["Martin, A.","Boyd, I., D."],"urls":{"Paper":"https://bibbase.org/service/mendeley/6476e386-2170-33cc-8f65-4c12ee0052f0/file/1c817bcb-b88f-432b-043d-ac2c74aacdc4/full_text.pdf.pdf","Website":"https://arc.aiaa.org/doi/abs/10.2514/1.A32847"},"biburl":"https://bibbase.org/service/mendeley/6476e386-2170-33cc-8f65-4c12ee0052f0","bibbaseid":"martin-boyd-stronglycoupledcomputationofmaterialresponseandnonequilibriumflowforhypersonicablation-2015","role":"author","keyword":["Arbitrary Lagrangian Eulerian","Boundary Layer","Courant Friedrichs Lewy","Freestream Mach Number","Heat Flux","Hypersonic Ablation","Hypersonic Aerothermodynamics","Nonequilibrium Flows","Pyrolysis","Stagnation Point"],"metadata":{"authorlinks":{}},"downloads":1},"bibtype":"article","biburl":"https://bibbase.org/service/mendeley/6476e386-2170-33cc-8f65-4c12ee0052f0","dataSources":["qwkM8ZucCwtxbnXfc","ya2CyA73rpZseyrZ8","2252seNhipfTmjEBQ"],"keywords":["arbitrary lagrangian eulerian","boundary layer","courant friedrichs lewy","freestream mach number","heat flux","hypersonic ablation","hypersonic aerothermodynamics","nonequilibrium flows","pyrolysis","stagnation point"],"search_terms":["strongly","coupled","computation","material","response","nonequilibrium","flow","hypersonic","ablation","martin","boyd"],"title":"Strongly Coupled Computation of Material Response and Nonequilibrium Flow for Hypersonic Ablation","year":2015,"downloads":1}