@article{
 title = {Modeling of near-continuum laminar boundary layer shocks using DSMC},
 type = {article},
 year = {2016},
 keywords = {DSMC,Hypersonic separated flows,Shock-wave boundary layer interactions},
 pages = {050004},
 volume = {1786},
 websites = {https://aip.scitation.org/doi/abs/10.1063/1.4967554},
 month = {11},
 publisher = {AIP Publishing LLCAIP Publishing},
 day = {15},
 id = {7d0ad86c-0087-3ef9-b547-77ab3d5d7b05},
 created = {2022-06-09T15:30:11.051Z},
 accessed = {2022-06-09},
 file_attached = {true},
 profile_id = {6476e386-2170-33cc-8f65-4c12ee0052f0},
 group_id = {5a9f751c-3662-3c8e-b55d-a8b85890ce20},
 last_modified = {2022-06-09T15:30:12.458Z},
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 private_publication = {false},
 abstract = {The hypersonic flow of nitrogen gas over a double wedge was simulated by the DSMC method using two-dimensional and three-dimensional geometries. The numerical results were compared with experiments...},
 bibtype = {article},
 author = {Tumuklu, Ozgur and Levin, Deborah A. and Gimelshein, Sergey F. and Austin, Joanna M.},
 doi = {10.1063/1.4967554},
 journal = {AIP Conference Proceedings},
 number = {1}
}

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