Open AccessUnsteady Characteristics of a Swept-Shock/Boundary-Layer Interaction at Mach 2
Author(s) -
Nishul Arora,
Lee Mears,
Farrukh Alvi
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.j058233
Subject(s) - mach number , boundary layer , shock (circulatory) , mechanics , mach wave , mach reflection , physics , flow (mathematics) , oblique shock , fin , swept wing , angle of attack , shock wave , materials science , aerodynamics , aerospace engineering , engineering , medicine
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