Model Parameter Estimation Method on Multichannel Structural Response from Turbulence Flutter Test

<table class="table-group" id="tab4"><tr><td><table class="table"><tr><td class="thead-hr" colspan="6"><hr/></td></tr><tr class="thead"><td class="align_left" colspan="2">All wing signal</td><td class="align_center" colspan="2">Left wing signal</td><td class="align_center" colspan="2">Right wing signal</td></tr><tr class="thead"><td class="align_left">Frequency (Hz)</td><td class="align_center">Damping ratio</td><td class="align_center">Frequency (Hz)</td><td class="align_center">Damping ratio</td><td class="align_center">Frequency (Hz)</td><td class="align_center">Damping ratio</td></tr><tr><td class="thead-hr" colspan="6"><hr/></td></tr><tr><td class="align_left">17.972</td><td class="align_center">13.881</td><td class="align_center">17.374</td><td class="align_center">10.581</td><td class="align_center">18.918</td><td class="align_center">12.114</td></tr><tr><td class="align_left">32.622</td><td class="align_center">5.764</td><td class="align_center">33.098</td><td class="align_center">5.340</td><td class="align_center">33.269</td><td class="align_center">5.226</td></tr><tr class="table-tr"><td colspan="6"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Modal parameter estimation results of the wing symmetrical position.</div>

International Journal of Aerospace Engineering

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Table 4

Table 4: Model Parameter Estimation Method on Multichannel Structural Response from Turbulence Flutter Test 