Numerical Simulation of Aircraft Icing with an Unsteady Thermodynamic Model considering the Development of Water Film and Ice Layer

Table 1

Boundary conditions for icing simulations.

Run no.	[m/s]	[K]	Angle of attack [°]	[g/m^3]	[μm]	[min]
R401	102.8	265.37	3.5	0.55	20	7
R402	102.8	263.71	3.5	0.55	20	7
R421	67.1	268.40	3.5	1.00	20	6
R422	67.1	266.74	3.5	1.00	20	6