Experimental Study on Flexible Deformation of a Flapping Wing with a Rectangular Planform

Table 1

Mechanical properties of the wing.

Parameters	Value
Carbon fiber rods
Elastic modulus	103.1 GPa
Poisson’s ratio	0.34
Density	1.5 g/cm^3
Polyester membrane skin
Elastic modulus	125.0 MPa
Density	1.4 g/cm^3