Research Article

A Gradient Stable Node-Based Smoothed Finite Element Method for Solid Mechanics Problems

Table 2

First 12 natural frequencies (104 Hz) of a cantilever beam.

No. of elementsNo. of nodesFEM-T3FEM-Q4NS-FEMGS-FEMReference FEM-Q4 (100 × 10)

(10 × 1) 10 4-node elements for FEM-Q4 and 20 triangular elements for other methods220.16920.09920.05760.13020.0824
0.91630.57910.32430.71610.4944
1.28691.28340.74411.28461.2824
2.18431.48300.98751.72301.3022
3.59422.61831.01122.85482.3663
3.83383.81401.13463.77283.6085
5.03353.88241.27833.99613.8442
6.24215.19241.57125.04174.9674
6.41546.23452.36975.90116.3960
7.59406.48463.26856.02776.4023
8.47907.70393.70646.49657.8853
8.70338.46323.86426.81628.9290

(20 × 2) 40 4-node elements for FEM-Q4 and 80 triangular elements for other methods630.11170.08700.06750.08470.0824
0.65390.51990.40320.50260.4944
1.28431.28301.05181.28221.2824
1.67481.36401.28101.30551.3022
2.95542.46851.64672.32742.3663
3.84243.74771.87863.47473.6085
4.38663.83782.78233.82413.8442
5.88365.13223.09264.67034.9674
6.37516.35853.67835.86016.3960
7.40466.57313.80896.29176.4023
8.82108.03424.05437.01207.8853
8.94118.81874.16058.09838.9290

(40 × 4) 160 4-node elements for FEM-Q4 and 320 triangular elements for other methods2050.09060.08350.07780.08140.0824
0.54090.50040.46540.48760.4944
1.28311.28271.21991.28011.2824
1.41611.31741.28181.28311.3022
2.55702.39261.66892.31752.3663
3.84333.64622.20123.51593.6085
3.87863.84313.25173.83913.8442
5.30875.01503.32704.80974.9674
6.39356.38833.83446.15316.3960
6.80936.45614.52486.36926.4023
8.34737.93984.64067.51417.8853
8.91838.90575.32758.85158.9290