Separation attenuation in swept shock wave–boundary-layer interactions using different microvortex generator geometries
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DOI: 10.1007/s00193-016-0690-8
Abstract: A numerical study is conducted to determine the effectiveness of six different microvortex generator geometries in controlling swept shock wave/boundary-layer interactions. The geometries considered are base ramp, base ramp with declining angle of $$45\,^{\circ }$$45∘,… read more here.
Keywords: generator geometries; shock; microvortex generator; shock wave ... See more keywords
Microvortex Generator Controlled Shock–Boundary Layer Interactions in Hypersonic Intake
Sign Up to like & getrecommendations! Published in 2021 at "Journal of Aerospace Engineering"
DOI: 10.1061/(asce)as.1943-5525.0001239
Abstract: AbstractThe occurrence of shock and boundary layer interactions (SBLIs) in aircraft-engine intakes often results in poor total pressure recovery, a degraded boundary layer, and, in worst cases, flo... read more here.
Keywords: layer interactions; microvortex generator; shock boundary; boundary layer ... See more keywords