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

Table 6

Performance influencing parameters of Design-3.

	Zone-1	Zone-2	Zone-3	Zone-4	Zone-5
Temperature	0	-25	-50	-75	-100
Diameter (m)	0.254	0.254	0.254	0.254	0.254
Velocity (m/s)	8	8	8	8	8
RPM	5000	5500	6000	6500	7000
	0.00040640	0.00036946	0.00033867	0.00031262	0.00029029
	2.4552096	3.2712276	4.2198021	5.1333224	6.0548878
	0.7452316	0.0933491	0.11058357	0.09135552	0.15078502
	1.97e-05	2.17e-05	2.35e-05	2.43e-05	2.47-05
	1.57e-10	5.64e-10	5.14e-10	4.54e-10	3.98e-10
	8.079026632	2.23e+100	2.462487318	2.667694594	2.872901871