Investigation of the Normal Blowing Approach to Controlling Wingtip Vortex Using LES

Table 1

Test case and grid information used for verification.

Test case	Case 1	Case 2	Case 3	Exp
Grid	Mesh 1	Mesh 2	Mesh 3	—
Along camber	523	711	1038	—
Along radial direction	91	96	126	—
Along span-wise direction	151	161	188	—
Along maximum wing thickness	97	121	131	—
Total/10^6	8.46	14.36	25.19	—
Axial velocity,	1.38	1.45	1.50	~1.53
Axial velocity,	1.33	1.40	1.46	~1.45