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Modal Analysis and Response Spectrum
Type: MD
Complété

Modal Analysis Techniques for Dynamic Response of Structures

Introduction

Modal analysis is a fundamental technique in structural dynamics, providing insight into the vibration characteristics of structures. By decomposing a structure's response into its constituent modes, engineers can predict how it will respond to various dynamic loads. This chapter delves into the techniques of modal analysis to elucidate the dynamic response of structures, followed by an exploration of response spectrum analysis in seismic engineering.

Modal Analysis: Fundamental Concepts

Modal Analysis is an analytical procedure that determines the natural frequencies, mode shapes, and modal damping ratios of a structure. It is crucial for understanding how structures will behave under dynamic loading conditions.

Natural Frequencies and Mode Shapes

  • Natural Frequencies: The frequencies at which a structure prefers to vibrate. These are inherent properties of the structure, dependent on its mass and stiffness distribution.
  • Mode Shapes: The deformation pattern of a structure at a particular natural frequency. Each mode shape represents a distinct pattern of motion.

Eigenvalue Problem

The core of modal analysis involves solving an eigenvalue problem derived from the equation of motion for undamped free vibration:

[ [M]{ \ddot{x} } + [K]{ x } = { 0 } ]

where ([M]) is the mass matrix, ([K]) is the stiffness matrix, and ({ x }) is the displacement vector. By assuming a solution of the form ({ x(t) } = { \phi } e^{i \omega t}), where ({ \phi }) is the mode shape vector and (\omega) is the natural frequency, the equation reduces to:

[ ([K] - \omega^2 [M]){ \phi } = { 0 } ]

The solution of this equation provides the eigenvalues ((\omega^2)) and eigenvectors (({ \phi })) of the system, representing the natural frequencies and mode shapes, respectively.

Modal Superposition Method

The modal superposition method is a technique used to predict the dynamic response of structures by expressing the response as a linear combination of its mode shapes. The equation of motion for a damped system is given by:

[ [M]{ \ddot{x} } + [C]{ \dot{x} } + [K]{ x } = { F(t) } ]

Using the modal superposition method, the displacement vector ({ x(t) }) can be expressed as a sum of modal contributions:

[ { x(t) } = \sum_{r=1}^{n} { \phi_r } q_r(t) ]

where ({ \phi_r }) is the r-th mode shape and (q_r(t)) is the modal coordinate. Substituting this into the equation of motion and applying orthogonality conditions leads to a set of uncoupled differential equations for each mode.

Damping in Modal Analysis

In real-world applications, damping plays a crucial role in the dynamic response of structures. Modal damping is often represented as a fraction of critical damping specific to each mode:

[ C_r = 2 \zeta_r \omega_r ]

where (\zeta_r) is the damping ratio for mode (r). This allows the inclusion of damping effects in modal analysis by modifying the decoupled equations to account for energy dissipation.

Response Spectrum Analysis in Seismic Engineering

Overview

Response spectrum analysis is a method used in seismic engineering to estimate the peak response of structures subjected to earthquake ground motions. It is based on the concept of response spectra, which plots the maximum response (e.g., displacement, velocity, or acceleration) of single-degree-of-freedom (SDOF) systems to a particular ground motion as a function of natural frequency or period.

Construction of Response Spectra

To construct a response spectrum, the ground motion is applied to an SDOF system with varying natural frequencies. The peak response is recorded for each frequency, resulting in a graph that provides critical information for assessing the seismic performance of structures.

Application in Multi-Degree-of-Freedom Systems

For multi-degree-of-freedom (MDOF) systems, the response spectrum method involves the following steps:

  1. Modal Analysis: Perform modal analysis to obtain natural frequencies and mode shapes of the structure.
  2. Spectral Ordinate Calculation: Use the response spectrum to determine the spectral acceleration, velocity, or displacement for each mode.
  3. Modal Response Calculation: Calculate the response for each mode using the spectral ordinates.
  4. Combination of Modal Responses: Combine the modal responses using methods such as the square root of the sum of squares (SRSS) or the complete quadratic combination (CQC) to obtain the total response.

Example

Consider a three-story building subjected to a seismic event. By performing modal analysis, the natural frequencies and mode shapes are determined. Using a response spectrum for the given seismic event, the spectral accelerations for these modes are obtained. The peak floor accelerations can then be estimated by combining the modal responses using an appropriate combination method.

Conclusion

Modal analysis and response spectrum analysis are indispensable techniques in the field of structural dynamics and seismic engineering. By understanding and applying these methods, engineers can predict and mitigate the dynamic responses of structures to various loading conditions, ensuring their safety and performance.

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