State-Space Adaptation of Unsteady Lifting Line Theory: Twisting/Flapping Wings of Finite Span
In this paper, a low-order state-space adaptation of the unsteady lifting line model has been analytically derived for a wing of finite aspect ratio, suitable for use in real-Time control of wake-dependent forces. Each discretization along the span has between 1-6 states to represent the local unste...
| Main Authors: | , , |
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| Format: | Article |
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American Institute of Aeronautics and Astronautics (AIAA)
2019
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| Online Access: | http://hdl.handle.net/1721.1/120112 https://orcid.org/0000-0002-1555-9136 https://orcid.org/0000-0002-4960-7060 |