Experimental Data for the 10 Degree Swept Wing (S10)

Raw data from the wind-tunnel experiments of the swept Pazy wing with 10 degrees of sweep (S10) . NASTRAN models for both LE and TE configurations. Sensors: 30 strain mesurements - 1000 Hz 2 rate gyros and 2 accelorametors ~ 680 Hz ~32 dispacements mesurements from a motion recovery system - 240 Hz Wind tunnel mesured dynamic pressure (DynP) and AoA at 10 KHz interpulated to 240 and 1000 Hz The data includes results from the following tests: 1) Ground vibration tests 2) Static conditions tests - stable AoA and airspeed for 20s 3) AoA sweep - quick AoA sweep at a constant airspeed 4) Responce to initial conditions - stable AoA and airspeed, wingtip wire was pulled and released 5)Flutter - constant AoA, airspeed is increased intill flutter. Flutter is stopped by the ditacment of the wingtip mass (see https://doi.org/10.5281/zenodo.16314906 ) 6)LCO - constant AoA, airspeed is increased intill flutter, made with thicker fuse/fixed weights *) Analyzed data will be uploaded in the future, a link will be added here