Experimental Investigation of Aerodynamics of Feather-Covered Flapping Wing

Table 1

Parameters of Nano17 sensor.

Force and torque sensor	Component	Range	Resolution	Stiffness
Nano17; SI-12-0.12; Φ17 × 15 mm	Fx	12 N	1/320 N	8.2 × 106 N/m
	Fy	12 N	1/320 N	8.2 × 106 N/m
	Fz	17 N	1/320 N	11 × 106 N/m
	Tx	120 Nmm	1/64 Nmm	240 Nm/rad
	Ty	120 Nmm	1/64 Nmm	240 Nm/rad
	Tz	120 Nmm	1/64 Nmm	380 Nm/rad