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Advances in Aerodynamics

Table 4 Maximum 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

2.51137

2.08185

4.05789

RBF

4.36848

3.90143

4.00810

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