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Flexible Wing MAV Aerodynamics Study by Tan Zhenyang is a document available to read on EtoBox.

5: Calibration setup with weights The calibration curves obtained were used to correct the raw data obtained from the wind tunnel experiments. This ensured that the forces registered were the true lift and drag values. 2.3 TEST PROCEDURE The wing models were tested at angles of attack ranging from -5° to 15° in increments of 2°. The free stream velocity was maintained at 6 m/s. Each model was tested individually and the lift and drag forces were recorded. The data was acquired for 10 seconds at each angle

Author

Tan Zhenyang

Language

EN