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