International Journal of Aerospace Engineering / 2021 / Article / Tab 5

Research Article

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

Table 5

Performance influencing parameters of Design-2.

Zone-1Zone-2Zone-3Zone-4Zone-5

Temperature0°C-25°C-50°C-75°C-100°C
Diameter (m)0.2540.2540.2540.2540.254
Velocity (m/s)88888
RPM50005500600065007000
0.000406400.000369460.000338670.000312620.00029029
6040768324.44982355.001458765.9845727.5842365
0.087562570.10586940.05866680.01358790.03658415
5013e-052.95e-052.78e-052.84e-053.10e-05
7.01e-077.67e-101.28e-062.53e-075.86e-07
0.044730002.57e-010.0011675080.0055676770.0002433480