Electrogasdynamic effect on small perturbation development in the boundary layer on a thin airfoil

DOI10.1007/BF01051095zbMath0602.76067MaRDI QIDQ1082196

A. V. Kazakov, A. P. Kuryachij

Publication date: 1986

Published in: Fluid Dynamics (Search for Journal in Brave)

zbMATH Keywords

boundary layer controlfree-stream velocityzero angle of attackcompressible gradient flowselectrogasdynamic method of boundary layer laminarizationleading edge of the airfoilperfect viscous gasplane subsonic flowthin symmetrical airfoil

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Ionized gas flow in electromagnetic fields; plasmic flow (76X05) Basic methods in fluid mechanics (76M99)

Related Items (1)

Localized forcing of the two-dimensional boundary layer by individual microdischarges in a plasma actuator

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