Efficacy Analysis of Thickness and Camber Size of Cross Section of the Stator on Hydrodynamic Parameters in Linear Jet Propulsion System

<table class="table-group" id="tab5"><tr><td><table class="table"><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr class="thead"><td class="align_left">Characteristic</td><td class="align_center">Number of blades</td><td class="align_center">Chord length (m)</td><td class="align_center">Diameter (m)</td></tr><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr><td class="align_left">Rotor</td><td class="align_center">5</td><td class="align_center">0.075</td><td class="align_center">0.2</td></tr><tr><td class="align_left">Stator</td><td class="align_center">7</td><td class="align_center">0.075</td><td class="align_center">0.2005</td></tr><tr class="table-tr"><td colspan="4"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>General information of the rotor and stator blade.</div>

Mathematical Problems in Engineering

tab5

Table 5

Table 5: Efficacy Analysis of Thickness and Camber Size of Cross Section of the Stator on Hydrodynamic Parameters in Linear Jet Propulsion System 