International Journal of Aerospace Engineering / 2021 / Article / Tab 4

Research Article

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-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
5.67923656.46525556.88448966.90860278.8464213
0.06892350.07920340.104893980.105339870.13501404
4.55e-054.28e-053.83e-053.27e-053.61e-05
5.52e-072.30e-062.30e-061.97e-062.17e-06
0.005329672.05e-130.0008985620.0008985620.000768898