Rotating Arm-Based Experimental Study on Droplet Behavior in the Shoulder Region of an Aircraft Aerodynamic Surface

Table 1

Dimensionless profile shape coordinates. “c” stands for the chord length. The leading edge coordinates are as follows: x/c = 0, z/c = 0.

x/c	z/c	x/c	z/c
1.000	0.000	0.241	0.200
0.937	0.014	0.211	0.196
0.877	0.028	0.183	0.191
0.818	0.044	0.157	0.183
0.762	0.059	0.133	0.173
0.707	0.076	0.110	0.162
0.655	0.093	0.090	0.150
0.604	0.110	0.072	0.136
0.556	0.127	0.056	0.121
0.510	0.143	0.042	0.105
0.465	0.158	0.030	0.089
0.423	0.171	0.020	0.072
0.383	0.183	0.012	0.055
0.344	0.192	0.006	0.041
0.308	0.198	0.002	0.032
0.274	0.200	0.000	0.000