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 |
Externí odkaz: |
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