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Wind Tunnel Test of a Highly Flexible, High Aspect Ratio Wing for a Future Research-UAV
>
Acceleration sensors attached to the surface of the wing for the modal test
Home
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Latest
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Technical articles
>
Wind Tunnel Test of a Highly Flexible, High Aspect Ratio Wing for a Future Research-UAV
>
Acceleration sensors attached to the surface of the wing for the modal test
Acceleration sensors attached to the surface of the wing for the modal test
Acceleration sensors attached to the surface of the wing for the modal test
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DLR (CC BY-NC-ND 3.0)
