Research Article

Structural Damping Effects on Dynamic Instability of Subtangentially Loaded and Shear Deformable Beck’s Columns

Table 6

Divergence and damped flutter loads of Beck’s columns for , 0.005, and 0.02 with variation of .

Subtangentiality, α0.00.10.20.30.3210.3540.40.4390.50.60.70.80.91.0
0.3170.3520.4330.488
0.3060.3450.4130.456

Undamped second flutter load, 19.4224.1328.7833.3449.35
17.6822.4127.3531.78
13.9618.81

Undamped first flutter load, (= externally damped flutter load, )19.4217.0816.4016.1616.0516.2616.7917.5918.6720.05
17.6815.3914.7314.5214.3714.4714.8415.4316.2017.16
13.9611.8911.2911.2111.0310.9411.0811.3511.7012.12

2% damped flutter load, 19.2217.0815.8614.5514.2014.1214.4014.9815.8517.03
17.4815.3914.2213.1712.8512.7112.9213.3614.0114.87
13.8011.8910.7410.3810.129.8579.94610.1710.4910.90

Internally damped flutter load, 19.4217.0815.8614.559.8709.3799.3059.52910.0510.94
17.4815.3914.2213.179.2378.7198.6578.8559.3039.983
13.9611.8910.7410.357.7977.2317.1947.3387.6378.083

2nd divergence load, 22.2121.1719.8918.2317.8117.0815.8614.559.870
19.9919.0517.9016.4016.0915.3914.2213.179.237
15.3814.6613.7712.5912.5111.8910.7410.357.797

1st divergence load, 2.4672.8303.3254.0554.2574.6265.2926.0999.870
2.4372.7953.2864.0124.1744.5605.2635.9529.237
2.3512.6973.1743.8913.9474.3615.2045.5097.797

The unmarked, , and marked values denote critical loads corresponding to , 0.005, and 0.02, respectively.