What is it about?
This study reveals the occurrence condition of static stall hysteresis in terms of the aspect ratio for low-aspect-ratio wings at a low Reynolds number. The key finding is that the stall hysteresis occurs when the aspect ratio is within a narrow region of the aspect ratio.
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Perspectives
The result in this publication is a new finding for static stall hysteresis for low-aspect-ratio wings. The result presumably can be applied not only for low Reynolds numbers, but also more broad range of the Reynolds number.
Makoto Mizoguchi
National Defense Academy of Japan
Read the Original
This page is a summary of: Aerodynamic Characteristics of Low-Aspect-Ratio Wings with Various Aspect Ratios in Low Reynolds Number Flows, TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, January 2016, Japan Society for Aeronautical and Space Sciences,
DOI: 10.2322/tjsass.59.56.
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