Open AccessUnsteady Characteristics of a Swept-Shock/Boundary-Layer Interaction at Mach 2
Author(s) -
Nishul Arora,
Lee Mears,
Farrukh S. Alvi
Publication year - 2019
Publication title -
aiaa journal/aiaa journal on disc
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 reflection , mach wave , aerospace engineering , physics , engineering , medicine