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Modeling the increase in aerodynamic efficiency for a thick (37.5% chord) airfoil with slot suction in vortex cells with allowance for the compressibility effect

Crossref DOI link: https://doi.org/10.1134/S1063785015010253

Published Online: 2015-02-28

Published Print: 2015-01

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

Authors

Isaev, S. A.

Baranov, P. A.

Sudakov, A. G.

Ermakov, A. M.
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