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

Table 4

Performance influencing parameters of Design-1.

	Zone-1	Zone-2	Zone-3	Zone-4	Zone-5
Temperature	0°C	-25°C	-50°C	-75°C	-100°C
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
	5.6792365	6.4652555	6.8844896	6.9086027	8.8464213
	0.0689235	0.0792034	0.10489398	0.10533987	0.13501404
	4.55e-05	4.28e-05	3.83e-05	3.27e-05	3.61e-05
	5.52e-07	2.30e-06	2.30e-06	1.97e-06	2.17e-06
	0.00532967	2.05e-13	0.000898562	0.000898562	0.000768898