Study on Transient Dynamics and Aerodynamic Characteristics of a New Type of High-Damping Four-Winged Rotating Parachute Inflation Process

Table 6

Comparison between numerical results and test results of rotation rate.

Case	Numerical rotation rate (r/s)	Test result of rotation rate (r/s)	Relative errors	The rate of (ω/v)
A	8.81	9.21	4.54	0.176
B	30.63	35.5	15.89	0.153
C	34.73	37.33	7.48	0.142
D	37.46	40.83	8.99	0.134