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Expansion of the range of critical mach numbers during control of transonic flow past a thick (20% chord) MQ airfoil with slot suction in a circular vortex flow

Crossref DOI link: https://doi.org/10.1134/S1063785014050174

Published Online: 2014-06-18

Published Print: 2014-05

Update policy: https://doi.org/10.1007/springer_crossmark_policy

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