Design and Analysis of Hybrid Fixed-Wing Type Flying Robot

Table 3

The results for structural and modal analysis.

Material	Young’s modulus	Parameters checked	Values
Carbon fiber	183 GPa	Deformation	3.1185-5 m
		Equivalent stress	0.46 MPa
		Deformation value for first and second mode shape	0
		Deformation value for third mode shape	0.0019 m
		Deformation value for fourth mode shape	1.379 m
		Deformation value for fifth mode shape	2.38 m
		Deformation value for sixth mode shape	2.745 m