Advances in Aerodynamics

Table 7 Maximum deformation under different operation conditions

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

	dx (mm)	dy (mm)	dz (mm)
CF	0.339	0.176	0.071
NP	0.863	0.574	0.146
NS	0.918	0.611	0.153

Back to article page