Structural Parameter Sensitivity Analysis of an Aircraft Anti-Icing Cavity Based on Thermal Efficiency

Table 1

Boundary condition types.

Boundary condition	Type
Jet hole	Pressure inlet
Export of the flow field	Pressure outlet
Outside skin surface	Convection wall
Inside skin surface	Coupled wall
Wall flute	Fixed temperature wall
Back shield	Adiabatic wall
Both sides of the baffle	Symmetry