A Computational Design Analysis of UAV’s Rotor Blade in Low-Temperature Conditions for the Defence Applications

Table 1

The geometry design of propellers.

Name	Diameter in m	Pitch	Amplitude	Frequency
Design-1	0.254	0.1778	N/A	N/A
Design-2	0.254	0.1778	N/A	N/A
Design-3	0.254	0.1778	1c	20w