Aeroelastic Optimization Design for High-Aspect-Ratio Wings with Large Deformation

Table 1

Overall parameter of wing model.

Parameter		Value	Unit
Span		1542	mm
Chord (root)		263	mm
Chord (tip)		71	mm
Elastic axis		40	% chord
Material of; beam: aluminum	Elastic modulus	70	Gpa
	Density	2790	Kg/m^3
	Tensile strength	524	MPa