Electrogasdynamic effect on small perturbation development in the boundary layer on a thin airfoil. (English. Russian original) Zbl 0602.76067
Fluid Dyn. 21, 19-26 (1986); translation from Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza 1986, No. 1, 25-33 (1986).
New, simple and economical methods of boundary layer control based on the use of electromagnetic forces are currently being sought. We examine the efficiency of the electrogasdynamic method of boundary layer laminarization in compressible gradient flows.
MSC:
| 76G25 | General aerodynamics and subsonic flows |
| 76X05 | Ionized gas flow in electromagnetic fields; plasmic flow |
| 76M99 | Basic methods in fluid mechanics |
Keywords:
plane subsonic flow; perfect viscous gas; thin symmetrical airfoil; zero angle of attack; free-stream velocity; leading edge of the airfoil; boundary layer control; electrogasdynamic method of boundary layer laminarization; compressible gradient flowsReferences:
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