Effect of a Bonded Patch on Aeroelastic Behavior of Cantilevered Plates

Table 4

Dimensionless amplitude of limit-cycle oscillations (w/h) of a cantilevered square plate in dimensionless coordinates (𝑥/𝑎,𝑦/𝑏)=(1,0.75) and dynamic pressure 𝜆=150 regarding the order of approximation polynomial series (𝑀_𝑖=𝑁_𝑖=𝑁) and number of in-plane and out-of-plane selected vibration mode shapes for reduced model (𝑛_in=𝑛_out=𝑛).

	𝑛=5	𝑛=6	𝑛=7	𝑛=8	𝑛=9
𝑁=5	0.537	0.538	0.544	0.609	0.541
𝑁=6	0.522	0.52	0.528	0.555	0.517
𝑁=7	0.522	0.522	0.528	0.555	0.52