International Journal of Aerospace Engineering / 2021 / Article / Tab 7

Research Article

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

Table 7

Operational zones vs. propeller efficiency.

TemperatureDesign-1Design-2Design-3

Zone-100.005329630.004734628.07902663
Zone-2-252.05e-132.257280042.25728004
Zone-3-500.000898560.001167512.46248732
Zone-4-750.000898560.005567682.66769459
Zone-5-1000.00076890.002433482.87290187