Direct Resistive Heating Simulation Tool for the Repair of Aerospace Structures through Composite Patches

Table 1

Material properties.

Id.	Material	Electrical conductivity			Thermal conductivity			ρC
		(Siemens/m)			(W/m °C)			(J/m^3°C)
		x	y	z	x	y	z
1	Bagging	0	0	0	0.069	0.069	0.069	446633.6
2	Fibreglass	0	0	0	0.58	0.58	0.58	1431000
3	Teflon	0	0	0	0.58	0.58	0.58	1431000
4	Dry fibre + epoxy	See Table 2			6.83	0.683	6.83	2022700
5	Thermal blanket	0	0	0	0.58	0.58	0.58	1431000