Patent ID: 11885234
Assignee: HONEYWELL INTERNATIONAL INC.
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F  B  Y | IPC F

Claim 15:
16. The method of claim 15, wherein the at least one local vortex generator array further comprises a second local vortex generator array defined on the suction side of the at least one airfoil and the hub, and wherein receiving, by the processor, the shape and location of the at least one local vortex generator array further comprises:
receiving, by the processor, a location of the first local vortex generator array on the suction side as between 1% chord to 50% chord in the chordwise direction and between greater than or equal to 60% span and 100% span in the spanwise direction; and
receiving, by the processor, a location of the second local vortex generator array on the suction side as between 1% chord to 50% chord in the chordwise direction and between less than or equal to 40% span and 0% span in the spanwise direction.