Performance Deterioration of Pitot Tubes Caused by In-Flight Ice Accretion: A Numerical Investigation

Table 1

Setup and inlet conditions of the airflow validation case over a 2D NACA0012 airfoil.

Geometry	NACA0012—1 m
Velocity	51 m/s
AoA	10°
Pressure	101,325 Pa
Density	1.18 kg/m^3
Temperature	300 K
Mach number	0.15
Reynolds number	3,500,000
Computational domain	O-type, diameter: 30 m
Mesh number	52,357