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Experimental study of laminar-turbulent transition on a swept wing with local boundary-layer suction at subsonic velocities |
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| Authors: | V F Babuev V I Biryukov V D Bokser A F Kiselev V G Mikeladze N V Nasedkin G K Shapovalov |
| Abstract: | 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 anglex=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. Moscow. Translated from Izvestiya Rossiiskoi Akademii Nauk, Mekhanika Zhidkosti i Gaza, No. 4, pp. 65–73, July–August, 1998. |
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