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https://doi.org/10.1061/(asce)as.1943-5525.0001174
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Cite Journal: Journal of Aerospace Engineering |  Publication Date: Jun 18, 2020 |
 Citations: 5 |
Affiliation: North University of China
AbstractThis paper presents a Volterra series reduced-order model method to evaluate aerodynamic forces of aircraft engine blade designs, whose shape changes during design and are always excited by...
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