Prediction of Dynamic Stability Using Mapped Chebyshev Pseudospectral Method

<table class="table-group" id="tab3"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_left">Properties</td><td class="align_center">Values</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">Freestream velocity</td><td class="align_center">8.84 m/s</td></tr><tr><td class="align_left">Reynolds number</td><td class="align_center">0.574 × 10<sup>6</sup>/m</td></tr><tr><td class="align_left">Amplitude</td><td class="align_center">4.16 and 8.33 deg.</td></tr><tr><td class="align_left">Reduced frequency</td><td class="align_center">0.1242</td></tr><tr><td class="align_left">Moment reference</td><td class="align_center">38% MAC</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Wind tunnel test conditions for forced oscillation.</div>

International Journal of Aerospace Engineering

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Table 3

Table 3: Prediction of Dynamic Stability Using Mapped Chebyshev Pseudospectral Method 