@article{
 title = {Flight Extrapolation of Plasma Wind Tunnel Stagnation Region Flowfield},
 type = {article},
 year = {2012},
 keywords = {Accurate Computational Fluid Dynamics,Binary Diffusion Coefficient,Boundary Layer Equations,Damköhler Numbers,Freestream Conditions,Heat Transfer,Hypersonic Flows,Shock Layers,Thermal Protection System,Wind Tunnels},
 pages = {493-499},
 volume = {20},
 websites = {https://arc.aiaa.org/doi/10.2514/1.17185},
 month = {5},
 publisher = {American Institute of Aeronautics and Astronautics Inc.},
 day = {23},
 id = {13805c96-2e27-3f48-9c88-c4b576cf2189},
 created = {2022-06-09T15:50:15.770Z},
 accessed = {2022-06-09},
 file_attached = {false},
 profile_id = {6476e386-2170-33cc-8f65-4c12ee0052f0},
 group_id = {5a9f751c-3662-3c8e-b55d-a8b85890ce20},
 last_modified = {2022-06-09T15:50:15.770Z},
 read = {false},
 starred = {false},
 authored = {false},
 confirmed = {false},
 hidden = {false},
 citation_key = {barbante:jtht:2012},
 private_publication = {false},
 abstract = {Development of reusable space vehicles requires a precise qualification of their thermal protection system materials. The catalytic properties are usually determined in plasma wind tunnels for test conditions relevant to the flight mission program. Therefore, for such a situation, it is important to have a methodology that allows the correct extrapolation of the ground test conditions to the real flight ones and vice-versa. The local heat transfer simulation concept presented in this paper is a possible strategy for accomplishing this task. Computational results show that the ground test conditions are indeed correctly extrapolated to the flight ones and a simple method of accounting for possible discrepancies between the two configurations is presented.},
 bibtype = {article},
 author = {Barbante, P. F. and Chazot, O.},
 doi = {10.2514/1.17185},
 journal = {Journal of Thermophysics and Heat Transfer},
 number = {3}
}

{"_id":"TgJaYmfrYQSobgvtK","bibbaseid":"barbante-chazot-flightextrapolationofplasmawindtunnelstagnationregionflowfield-2012","author_short":["Barbante, P., F.","Chazot, O."],"bibdata":{"title":"Flight Extrapolation of Plasma Wind Tunnel Stagnation Region Flowfield","type":"article","year":"2012","keywords":"Accurate Computational Fluid Dynamics,Binary Diffusion Coefficient,Boundary Layer Equations,Damköhler Numbers,Freestream Conditions,Heat Transfer,Hypersonic Flows,Shock Layers,Thermal Protection System,Wind Tunnels","pages":"493-499","volume":"20","websites":"https://arc.aiaa.org/doi/10.2514/1.17185","month":"5","publisher":"American Institute of Aeronautics and Astronautics Inc.","day":"23","id":"13805c96-2e27-3f48-9c88-c4b576cf2189","created":"2022-06-09T15:50:15.770Z","accessed":"2022-06-09","file_attached":false,"profile_id":"6476e386-2170-33cc-8f65-4c12ee0052f0","group_id":"5a9f751c-3662-3c8e-b55d-a8b85890ce20","last_modified":"2022-06-09T15:50:15.770Z","read":false,"starred":false,"authored":false,"confirmed":false,"hidden":false,"citation_key":"barbante:jtht:2012","private_publication":false,"abstract":"Development of reusable space vehicles requires a precise qualification of their thermal protection system materials. The catalytic properties are usually determined in plasma wind tunnels for test conditions relevant to the flight mission program. Therefore, for such a situation, it is important to have a methodology that allows the correct extrapolation of the ground test conditions to the real flight ones and vice-versa. The local heat transfer simulation concept presented in this paper is a possible strategy for accomplishing this task. Computational results show that the ground test conditions are indeed correctly extrapolated to the flight ones and a simple method of accounting for possible discrepancies between the two configurations is presented.","bibtype":"article","author":"Barbante, P. F. and Chazot, O.","doi":"10.2514/1.17185","journal":"Journal of Thermophysics and Heat Transfer","number":"3","bibtex":"@article{\n title = {Flight Extrapolation of Plasma Wind Tunnel Stagnation Region Flowfield},\n type = {article},\n year = {2012},\n keywords = {Accurate Computational Fluid Dynamics,Binary Diffusion Coefficient,Boundary Layer Equations,Damköhler Numbers,Freestream Conditions,Heat Transfer,Hypersonic Flows,Shock Layers,Thermal Protection System,Wind Tunnels},\n pages = {493-499},\n volume = {20},\n websites = {https://arc.aiaa.org/doi/10.2514/1.17185},\n month = {5},\n publisher = {American Institute of Aeronautics and Astronautics Inc.},\n day = {23},\n id = {13805c96-2e27-3f48-9c88-c4b576cf2189},\n created = {2022-06-09T15:50:15.770Z},\n accessed = {2022-06-09},\n file_attached = {false},\n profile_id = {6476e386-2170-33cc-8f65-4c12ee0052f0},\n group_id = {5a9f751c-3662-3c8e-b55d-a8b85890ce20},\n last_modified = {2022-06-09T15:50:15.770Z},\n read = {false},\n starred = {false},\n authored = {false},\n confirmed = {false},\n hidden = {false},\n citation_key = {barbante:jtht:2012},\n private_publication = {false},\n abstract = {Development of reusable space vehicles requires a precise qualification of their thermal protection system materials. The catalytic properties are usually determined in plasma wind tunnels for test conditions relevant to the flight mission program. Therefore, for such a situation, it is important to have a methodology that allows the correct extrapolation of the ground test conditions to the real flight ones and vice-versa. The local heat transfer simulation concept presented in this paper is a possible strategy for accomplishing this task. Computational results show that the ground test conditions are indeed correctly extrapolated to the flight ones and a simple method of accounting for possible discrepancies between the two configurations is presented.},\n bibtype = {article},\n author = {Barbante, P. F. and Chazot, O.},\n doi = {10.2514/1.17185},\n journal = {Journal of Thermophysics and Heat Transfer},\n number = {3}\n}","author_short":["Barbante, P., F.","Chazot, O."],"urls":{"Website":"https://arc.aiaa.org/doi/10.2514/1.17185"},"biburl":"https://bibbase.org/service/mendeley/6476e386-2170-33cc-8f65-4c12ee0052f0","bibbaseid":"barbante-chazot-flightextrapolationofplasmawindtunnelstagnationregionflowfield-2012","role":"author","keyword":["Accurate Computational Fluid Dynamics","Binary Diffusion Coefficient","Boundary Layer Equations","Damköhler Numbers","Freestream Conditions","Heat Transfer","Hypersonic Flows","Shock Layers","Thermal Protection System","Wind Tunnels"],"metadata":{"authorlinks":{}}},"bibtype":"article","biburl":"https://bibbase.org/service/mendeley/6476e386-2170-33cc-8f65-4c12ee0052f0","dataSources":["qwkM8ZucCwtxbnXfc"],"keywords":["accurate computational fluid dynamics","binary diffusion coefficient","boundary layer equations","damköhler numbers","freestream conditions","heat transfer","hypersonic flows","shock layers","thermal protection system","wind tunnels"],"search_terms":["flight","extrapolation","plasma","wind","tunnel","stagnation","region","flowfield","barbante","chazot"],"title":"Flight Extrapolation of Plasma Wind Tunnel Stagnation Region Flowfield","year":2012}