AIAA SCITECH 2023 Forum 2023
DOI: 10.2514/6.2023-0649
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Strip theory approach to corner effects in shock-wave boundary layer interactions

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Cited by 4 publications
(1 citation statement)
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“…2a. This deflection angle was selected such that its dimensionless interaction intensity (as defined by Souverein [18]) matches that of other recent compression corner studies conducted at Mach 2.5 [19,20]. Furthermore, the predicted size of the separation according to the model proposed by Souverein [18] is sufficiently large that it would typically be thought to require control.…”
Section: A Wind Tunnel Setupmentioning
confidence: 99%
“…2a. This deflection angle was selected such that its dimensionless interaction intensity (as defined by Souverein [18]) matches that of other recent compression corner studies conducted at Mach 2.5 [19,20]. Furthermore, the predicted size of the separation according to the model proposed by Souverein [18] is sufficiently large that it would typically be thought to require control.…”
Section: A Wind Tunnel Setupmentioning
confidence: 99%