Steady and unsteady stall are studied on a rectangular wing in normal flow. The wing is allowed to oscillate in pitch around the fore quarter chord. Experiments performed at the S 2 wind-tunnel in Chalais-Meudon with a rectangular wing and a wind velocity of 95 m/s are in good agreement with the results obtained from the theory developed.
Unsteady Three-Dimensional Stall on a Rectangular Wing
1988
15 pages
Report
Keine Angabe
Englisch
Dynamic stall on a three-dimensional rectangular wing
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