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Advances in Aerodynamics

Table 2 Comparisons of deformation calculated by FEA program and ANSYS Workbench

From: Static aeroelasticity analysis of a rotor blade using a Gauss-Seidel fluid-structure interaction method

 

\(\delta\) (dx)

\(\delta\) (dy)

\(\delta\) (dz)

CF

0.903%  

1.274%  

0.845%  

CF+AL

1.928%  

2.418%  

1.843%  

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