Experimental study of laminar-turbulent transition on a swept wing with local boundary-layer suction at subsonic velocities.

Autor: Babuev, V., Biryukov, V., Bokser, V., Kiselev, A., Mikeladze, V., Nasedkin, N., Shapovalov, G.
Zdroj: Fluid Dynamics; Jul1998, Vol. 33 Issue 4, p519-525, 7p
Abstrakt: The effect of local suction of the boundary layer gas near the leading edge of the upper surface of a swept wing (with the sweep angle x=35°) on the extent of the laminar flow region is studied on a large half-model at subsonic velocities. Various experimental methods were used. The data are subjected to a comparative analysis. [ABSTRACT FROM AUTHOR]
Databáze: Complementary Index