Effect of a Bonded Patch on Aeroelastic Behavior of Cantilevered Plates

Table 5

Dimensionless coordinates of points selected on the plate free edge for studying amplitude of limit-cycle oscillations.

	Point 1	Point 2	Point 3	Point 4	Point 5
(𝑥/𝑎,𝑦/𝑏)	(1,0)	(1,0.25)	(1,0.5)	(1,0.75)	(1,1)