@article{
 title = {Inviscid Hypersonic Flow Over Blunt-Nosed Slender Bodies},
 type = {article},
 year = {1957},
 keywords = {Air Transportation,Angle of Attack,Drag Coefficient,Guggenheim Aeronautical Laboratory,Hypersonic Speed,Hypersonic Wind Tunnels,Inviscid Hypersonic Flow,Leading Edges,Pressure Coefficient,Shock Wave Interaction},
 pages = {195-202},
 volume = {24},
 month = {3},
 publisher = {American Institute of Aeronautics and Astronautics (AIAA)},
 day = {29},
 id = {ce273fb5-7b7c-3ab2-8dfc-3ff0c9d86e06},
 created = {2021-05-28T23:42:04.823Z},
 accessed = {2021-05-28},
 file_attached = {false},
 profile_id = {6476e386-2170-33cc-8f65-4c12ee0052f0},
 group_id = {5a9f751c-3662-3c8e-b55d-a8b85890ce20},
 last_modified = {2021-07-23T21:07:17.127Z},
 read = {false},
 starred = {false},
 authored = {false},
 confirmed = {false},
 hidden = {false},
 citation_key = {lees:jas:1957},
 private_publication = {false},
 bibtype = {article},
 author = {Lees, Lester and Kubota, Toshi},
 doi = {10.2514/8.3803},
 journal = {Journal of the Aeronautical Sciences},
 number = {3}
}

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