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Investigation of the development of unsteady flow separation from a model swept wing |
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| Authors: | I V Kolin V G Markov V L Sukhanov T I Trifonova D V Shukhovtsov |
| Abstract: | The results of an experimental wind-tunnel investigation of the flow patterns on the swept wing of a model aircraft realized for pitching oscillations with an amplitude A α = 5° with respect to setup angles of attack α0 = 10 and 16° are presented. |
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