Advances in Aerodynamics

Table 1 Measurement range and calibration results of the balance

From: Effect of vortex generator spanwise height distribution pattern on aerodynamic characteristics of a straight wing

Item	Y	Mz	X	Mx	Z	My
Design load (N, N·m)	1200	200	600	100	150	100
Calibration load (N, N·m)	1200	120	400	40	300	30
Absolute error (N, N·m)	2.4	0.24	0.8	0.08	0.6	0.06
Accuracy (%)	0.2	0.2	0.2	0.2	0.2	0.2
Precision (%)	0.02	0.02	0.02	0.06	0.02	0.02

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