International Journal of Aerospace Engineering / 2021 / Article / Tab 2

Research Article

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

Table 2

The parameters of the grid generation.

Use advance size functionCurvature

Relevance centreCoarse
Curvature normal angle70.9
Min size0.589180
Max face size50.9180
Max size117.840
Growth rate1.850
Minimum edge length