Abstract
Structural Deformation-Based Computational Method for Static Aeroelasticity of High-Aspect-Ratio Wing Model in Pressurized Wind Tunnel
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https://doi.org/10.4208/aamm.oa-2017-0342
Publication Date: Jun 1, 2018 | |
Citations: 2 |
Structural Deformation-Based Computational Method for Static Aeroelasticity of High-Aspect-Ratio Wing Model in Pressurized Wind Tunnel
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