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Wind Tunnel Test of a Highly Flexible, High Aspect Ratio Wing for a Future Research-UAV
>
Span (b) and wing area (F) for calculation of the wing‘s aspect ratio
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Latest
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Technical articles
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Wind Tunnel Test of a Highly Flexible, High Aspect Ratio Wing for a Future Research-UAV
>
Span (b) and wing area (F) for calculation of the wing‘s aspect ratio
Span (b) and wing area (F) for calculation of the wing‘s aspect ratio
Span (b) and wing area (F) for calculation of the wing‘s aspect ratio
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DLR (CC BY-NC-ND 3.0)
