One of the first concepts that is being taught in earthquake engineering classes is determination of dynamic properties of structures such as frequency and period. Under the action of earthquakes or external forces, the structure moves, and this movement is heavily influenced by its dynamic properties.
With the advent of industry softwares such as MIDAS Gen and open-source, research-based analysis softwares, calculation of these properties can now be done in seconds at best. However, many structural engineers, the author himself included, believe that the user should be able to manually calculate or at least understand the theoretical concepts these softwares use to check the accuracy of results and to better understand the structural model.
In this article, we will talk about the basic concepts in the structural dynamics of multiple degrees-of-freedom (MDOF) systems under free vibration. Softwares use concepts way more advanced than those presented here. Nevertheless, basic concepts are useful as the user is given a feel of how the structure (and the software he uses) works.
But first, some definitions.
For the purposes of simplifying equations, consider a one-bay, two-story frame structure subject to free vibration as shown in Figure 1 below. Other structures can be analyzed in a similar manner.
We will assume the following.
The equivalent lumped mass model and free-body diagram for each floor are also shown. We will designate all quantities related to the first-floor level with the subscript “1”, and the second-floor level with the subscript “2”.
Applying equilibrium equations for each floor and simplifying, we get the system
In matrix form, we can write the above system as
[m]{u ̈ }+[c]{u ̇ }+[k]{u}={0}
which is very similar in form to that of SDOF systems. Here, [m], [c] and [k] are called mass, damping and stiffness matrices, respectively.
A special case worth considering is when we neglect damping in the structure, i.e. [c]=[0]. We have the equation
By making the substitution {u ̈ }=-ω_n^2 {u}, we have the eigenvalue problem
Because {𝑢} is nonzero, the only case this equation is true is when
Solving this equation gives us 𝑁 values of frequencies 𝜔𝑛, which we call the modal frequencies of the structure. Usually, these values are arranged in increasing order, with the smallest one assigned to mode 1, or the fundamental mode of vibration. Now, we can substitute each modal frequency back to the eigenvalue problem and then get its corresponding value of{𝑢}. This {𝑢} is not exactly the actual displacement of the structure; rather, it shows the displacement of each floor relative to a certain value when the structure is subjected to a frequency 𝜔𝑛. In other words, it quantitatively shows how the structure looks like, given 𝜔𝑛. This is called the mode shape of the structure and is denoted by {𝜙𝑖 }, where 𝑖 is the 𝑖th mode. Usually, the topmost floor of the structure is assigned a unit displacement, in which case the mode shapes that we will obtain are called normal mode shapes. From this, we can get the mode shape matrix
Finally, some additional quantities. We have the modal mass matrix, given by
We also have the modal participation factor
As an example, consider a three-story structure shown in Figures 2 to 5 below.
You can check more of these details in the download file.
Estrada, H., & Lee, L. S. (2017b). Introduction to earthquake engineering. CRC Press.
Cimellaro, G. P., & Marasco, S. (2018). Introduction to dynamics of structures and earthquake engineering. Springer.
Association of Structural Engineers of the Philippines, Inc. (2019). National Structural Code of the Philippines 2015 (7th ed., Vol. 1). (Original work published 2015)
Saito, T. (2015). STERA 3D User Manual. https://rc.ace.tut.ac.jp/saito/Software/STERA_3D/STERA3D_user_manual.pdf
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