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Advances in Aerodynamics

Table 5 Average relative error in each direction

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

 

\(\delta x\) (%)

\(\delta y\) (%)

\(\delta z\) (%)

LIWDR

2.019E-002

2.515E-002

2.939E-002

RBF

1.785E-002

2.674E-002

4.159E-002

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