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="tab1"><tr><td><table class="table"><tr><td class="thead-hr" colspan="8"><hr/></td></tr><tr class="thead"><td class="align_left">Duct (A)</td><td class="align_center">Type of duct</td><td class="align_center">Propeller section series</td><td class="align_center">Number of blades</td><td class="align_center">Propeller diameter</td><td class="align_center">P/D<sub><i>R</i></sub> ratio</td><td class="align_center">Expanded area ratio</td><td class="align_center">Hub diameter ratio</td></tr><tr><td class="thead-hr" colspan="8"><hr/></td></tr><tr><td class="align_left">19</td><td class="align_center">Accelerating</td><td class="align_center">Kaplan</td><td class="align_center">4</td><td class="align_center">0.2</td><td class="align_center">1</td><td class="align_center">0.7</td><td class="align_center">0.2</td></tr><tr class="table-tr"><td colspan="8"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Geometric specifications for propeller ka4.70 with duct 19A [<a href="/journals/mpe/2020/5861948/#B20" target="_blank">20</a>].</div>

Mathematical Problems in Engineering

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Table 1

Table 1: Efficacy Analysis of Thickness and Camber Size of Cross Section of the Stator on Hydrodynamic Parameters in Linear Jet Propulsion System 