External Aerodynamics Simulations in a Rotating Frame of Reference

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</svg> contours and streamlines comparison for rotating NACA 0012 airfoil at Mach = 0.2 and <i>α</i> = 0°: (a) present work, <svg height="16" id="M47" style="vertical-align:-2.29482pt" version="1.1" viewbox="0 0 56.25 16" width="56.25" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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</svg>, (b) Limache [<a href="/journals/ijae/2014/654037/#B10">7</a>], <svg height="16" id="M48" style="vertical-align:-2.29482pt" version="1.1" viewbox="0 0 56.25 16" width="56.25" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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</svg>.</table>

International Journal of Aerospace Engineering

External Aerodynamics Simulations in a Rotating Frame of Reference

Figure 2