A Computational Design Analysis of UAV’s Rotor Blade in Low-Temperature Conditions for the Defence Applications

<div class="floats-full-page floats-full-page-figure"><h2>Figure 29</h2><div class="floats-full-page-caption"><div>Performance influencing parameters of Design-1.</div></div><div class="floats-full-page-content"><table class="figure-group"><tr class="fig-image"><td><object data="https://static-01.hindawi.com/articles/ijae/volume-2021/8843453/figures/8843453.fig.0029.svgz" name="8843453.fig.0029" type="image/svg+xml"></object></td></tr></table></div></div>

Figure 29 | A Computational Design Analysis of UAV’s Rotor Blade in Low-Temperature Conditions for the Defence Applications

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Figure 29: A Computational Design Analysis of UAV’s Rotor Blade in Low-Temperature Conditions for the Defence Applications

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Figure 29

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<p><em>International Journal of Aerospace Engineering </em>serves the international aerospace engineering community through the dissemination of scientific knowledge on practical engineering and design methodologies pertaining to aircraft and space vehicles.</p>


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<p>Chief Editor, Professor Zhao, is based at the University of Canterbury and his research interests include applying theoretical, numerical and experimental approaches to study combustion instability, thermoacoustics and aerodynamics.</p>


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