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Nozzle Geometry Effects on Corner Boundary Layers in Supersonic Wind Tunnels
Author(s) -
Kshitij Sabnis,
Holger Babinsky
Publication year - 2019
Publication title -
aiaa journal
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.828
H-Index - 158
eISSN - 1081-0102
pISSN - 0001-1452
DOI - 10.2514/1.j058310
Subject(s) - transonic , aerodynamics , supersonic speed , boundary layer , wind tunnel , aerospace engineering , hypersonic speed , shock wave , geometry , physics , geology , engineering , mathematics

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