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  5. Implementing a Partitioned Algorithm for Fluid-Structure Interaction of Flexible Flapping Wings within Overture
 
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Implementing a Partitioned Algorithm for Fluid-Structure Interaction of Flexible Flapping Wings within Overture

Source
Presented at the 10th Symposium on Overset Composite Grids and Solution Technology, NASA Ames Research Centre, Moffett Field
Date Issued
2010-09-20
Author(s)
Chandar, Dominic D. J.
Murali, Damodaran
URI
https://d8.irins.org/handle/IITG2025/31147
Subjects
Airfoil
Fluid-Structure
Partitioned Algorithm
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