Numerical Calculations on the Unsteady Aerodynamic Force of the Tilt-Rotor Aircraft in Conversion Mode

<table class="table-group" id="tab1"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_left">Dynamic mesh method</td><td class="align_center">Maximum tilt angle (°)</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">IDW</td><td class="align_center">48</td></tr><tr><td class="align_left">RBF</td><td class="align_center">81</td></tr><tr><td class="align_left">Present method</td><td class="align_center">Greater than 90</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Comparison on deformation ability.</div>

International Journal of Aerospace Engineering

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Table 1

Table 1: Numerical Calculations on the Unsteady Aerodynamic Force of the Tilt-Rotor Aircraft in Conversion Mode 