Problem description
A simple multiple-degree-of-freedom spring-mass system is used to demonstrate the capability of using residual modes to obtain high solution accuracy. The model consists of 4 masses and 5 springs, as shown in Figure 1. The assembled mass and stiffness matrices are as follows:
The mass for node 4 is set to half the value of the other three nodes so as to have four distinct modes for the system. A spatial loading of unit force R is applied to node 3 in the y-direction, where
The eigenfrequencies and corresponding eigenmodes are given in the following table:
Mode No. | Frequency (Hz) | Nodal Eigendisplacements | |||
---|---|---|---|---|---|
Node 1 | Node 2 | Node 3 | Node 4 | ||
1 | 10.155 | 0.39948 | 0.63631 | 0.61408 | 0.03418 |
2 | 20.222 | 0.68548 | 0.26428 | –0.58359 | –0.48927 |
3 | 28.258 | 0.60461 | –0.69678 | 0.19839 | 0.46815 |
4 | 34.963 | 0.07056 | –0.19939 | 0.49292 | –1.19360 |
The spatial loading is applied harmonically with an excitation frequency of 3 Hz to verify the steady-state response of the system. The single residual mode corresponding to the excitation load is included in the projected basis. A modal damping factor of 0.02 is applied to all the modes including the residual modes.