@article{
 title = {Evaluation of Computational Modeling of Electron Transpiration Cooling at High Enthalpies},
 type = {article},
 year = {2017},
 pages = {283-293},
 volume = {31},
 month = {4},
 publisher = {American Institute of Aeronautics and Astronautics Inc.},
 day = {26},
 id = {2d923798-40a6-3811-a986-ed0476a195da},
 created = {2021-01-05T20:43:34.906Z},
 accessed = {2021-01-04},
 file_attached = {true},
 profile_id = {6476e386-2170-33cc-8f65-4c12ee0052f0},
 group_id = {5a9f751c-3662-3c8e-b55d-a8b85890ce20},
 last_modified = {2021-12-28T16:46:16.995Z},
 read = {false},
 starred = {false},
 authored = {false},
 confirmed = {false},
 hidden = {false},
 citation_key = {hanquist:jtht:2017},
 private_publication = {false},
 abstract = {Amodeling approach for electron transpiration cooling of high-enthalpy flight is evaluated through comparison to a set of experiments performed in a plasma arc tunnel for air and argon. The comparisons include air and argon flow at high enthalpies (27.9 and 11.6 MJ/kg, respectively), with a Mach number of 2.5 to 3. The conversion of the reported enthalpies and Mach numbers to freestream temperatures and velocities is discussed. The numerical approach is described, including implementation of a thermionic emission boundary condition and an electric field model. Also described is the implementation of a finite-rate chemistry model for argon ionization. Materials with different electron emission properties are also investigated, including graphite and tungsten. The comparisons include two different geometries with different leading-edge radii. The numerical results produce a wide range of emitted current due to the uncertainties in freestream conditions and emissive material properties, but they still agree well with the experimental measurements.},
 bibtype = {article},
 author = {Hanquist, Kyle M. and Alkandry, Hicham and Boyd, Iain D.},
 doi = {10.2514/1.T4932},
 journal = {Journal of Thermophysics and Heat Transfer},
 number = {2},
 keywords = {etc}
}

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