Design and Analysis of Propeller for High-Altitude Search and Rescue Unmanned Aerial Vehicle

<table class="table-group" id="tab4"><tr><td><table class="table"><tr><td class="thead-hr" colspan="5"><hr/></td></tr><tr class="thead"><td class="align_left">Altitude</td><td class="align_center">Analytical</td><td class="align_center">Numerical</td><td class="align_center">Experimental (off-design)</td><td class="align_center">Remarks</td></tr><tr><td class="thead-hr" colspan="5"><hr/></td></tr><tr><td class="align_left">1400 m</td><td class="align_center">1.70 N</td><td class="align_center">2.27 N</td><td class="align_center">0.92 N</td><td class="align_center">At 2679 RPM</td></tr><tr class="table-tr"><td colspan="5"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Comparison of thrust generation.</div>

International Journal of Aerospace Engineering

tab4

Table 4

Table 4: Design and Analysis of Propeller for High-Altitude Search and Rescue Unmanned Aerial Vehicle 