International Journal of Aerospace Engineering / 2021 / Article / Tab 6

Research Article

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

Temperature0-25-50-75-100
Diameter (m)0.2540.2540.2540.2540.254
Velocity (m/s)88888
RPM50005500600065007000
0.000406400.000369460.000338670.000312620.00029029
2.45520963.27122764.21980215.13332246.0548878
0.74523160.09334910.110583570.091355520.15078502
1.97e-052.17e-052.35e-052.43e-052.47-05
1.57e-105.64e-105.14e-104.54e-103.98e-10
8.0790266322.23e+1002.4624873182.6676945942.872901871