International Journal of Aerospace Engineering / 2021 / Article / Tab 1

Research Article

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

Table 1

The geometry design of propellers.

NameDiameter in mPitchAmplitudeFrequency

Design-10.2540.1778N/AN/A
Design-20.2540.1778N/AN/A
Design-30.2540.17781c20w