Prediction of Lift Coefficient for Tandem Wing Configuration or Multiple-Lifting-Surface System Using Prandtl’s Lifting-Line Theory

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/3104902/figures/3104902.fig.0016a.svgz" name="3104902.fig.0016a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Incidence angle of the hind wing</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/3104902/figures/3104902.fig.0016b.svgz" name="3104902.fig.0016b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Incidence angle of the fore wing</td></tr></table>

<div>Effect of incidence angle on section lift coefficient for tandem wing configuration.</div>

International Journal of Aerospace Engineering

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Figure 16

Figure 16: Prediction of Lift Coefficient for Tandem Wing Configuration or Multiple-Lifting-Surface System Using Prandtl’s Lifting-Line Theory 