Advances in Aerodynamics

Table 6 Converged FSI solutions

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

	dx (mm)	dy (mm)	dz (mm)	\(\pi\)	\(\eta\)
\(F_{100}\)	0.863	0.574	0.146	2.087	0.872
\(F_{400}\)	0.863	0.574	0.146	2.087	0.871
\(F_{800}\)	0.863	0.573	0.146	2.087	0.871

Back to article page