Instabilities in shock-wave–boundary-layer interactions at Mach 6
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DOI: 10.1017/jfm.2025.10597
Abstract: Abstract The flow instabilities in shock-wave–boundary-layer interactions at Mach 6 are comprehensively investigated through compression corner and incident shock cases. The boundary of global stability and the characteristics of globally unstable modes are determined by… read more here.
Keywords: wave boundary; layer interactions; instabilities shock; interactions mach ... See more keywords