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

Table 2

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

Geometry	NACA0012—0.5334 m
Velocity	102.80 m/s
AoA	4°
Pressure	100,920 Pa
Density	1.46 kg/m^3
Temperature	262.04 K
MVD	20 μm
LWC	0.55 g/m^3
Reynolds number	5,100,000
Computational domain	O-type, diameter -16 m
Mesh number	49,176