Modal Testing & Experimental Modal Analysis

Interactive Lecture

Frequency Response Functions, Curve Fitting, and Modal Parameters

by Dr Arnaldo Delli Carri

Introduction to Modal Testing

Modal testing is an experimental technique used to identify the dynamic characteristics of structures. By measuring the structure's response to excitation, we can extract modal parameters: natural frequencies, damping ratios, and mode shapes. These parameters form the foundation for structural dynamics analysis, validation of finite element models, and troubleshooting vibration problems.

Key objectives of modal testing:

Testing Approaches

Measurement Chain

A complete modal test requires: (1) Excitation device (hammer or shaker), (2) Force transducer to measure input, (3) Accelerometers to measure response, (4) Data acquisition system, and (5) Modal analysis software for parameter extraction.

Frequency Response Functions (FRF)

The FRF Concept

The Frequency Response Function (FRF) is the ratio of output (response) to input (force) in the frequency domain. It completely characterises the linear dynamic behaviour of a structure at a given location.

FRF Definition:

\[H(\omega) = \frac{X(\omega)}{F(\omega)}\]

Where:

For a SDOF system:

\[H(\omega) = \frac{1}{k - m\omega^2 + j c\omega} = \frac{1/k}{1 - r^2 + j(2\zeta r)}\]

Where \(r = \omega/\omega_n\) and \(\zeta\) is the damping ratio

FRF Representations:

System Parameters

25
2.0
10

FRF Display Type:

Derived Parameters

Stiffness: \(k = m\omega_n^2 =\) 0 N/m

Damping coeff: \(c = 2\zeta m\omega_n =\) 0 Ns/m

Peak at \(f_n\); phase is −90° at resonance for the displayed FRF type; Nyquist traces a circle for SDOF.

MDOF Systems and Modal Superposition

Multi-Degree-of-Freedom FRFs

Real structures have many modes. The measured FRF is a superposition of individual modal contributions, each with its own frequency, damping, and mode shape.

MDOF FRF (Modal Superposition):

\[H_{jk}(\omega) = \sum_{r=1}^{N} \frac{\Phi_{jr}\Phi_{kr}}{m_r(\omega_{r}^2 - \omega^2 + j2\zeta_r\omega_r\omega)}\]

Where:

Residue Form:

\[H_{jk}(\omega) = \sum_{r=1}^{N} \left[\frac{A_{jk}^r}{j\omega - \lambda_r} + \frac{\bar{A}_{jk}^r}{j\omega - \bar{\lambda}_r}\right]\]

Where \(A_{jk}^r\) is the modal residue and \(\lambda_r = -\zeta_r\omega_r + j\omega_r\sqrt{1-\zeta_r^2}\) is the complex pole

Multi-Mode System

Mode 1:

20
1.5
1.0

Mode 2:

60
2.0
0.5

Mode 3:

110
2.5
0.3

Peak Identification:

Peaks appear at each natural frequency. Well-separated modes (spacing > 2× bandwidth) are easier to identify accurately.

Modal density: 1.5 modes / 100 Hz

Modal Parameter Extraction

Curve Fitting Methods

Modal parameters are extracted from measured FRFs using curve fitting algorithms. Different methods suit different situations based on mode separation and data quality.

Peak Picking (Simplest):

\[f_n = f_{\text{peak}}\]

Damping from the peak amplitude (quality factor \(Q\)):

\[\zeta \approx \frac{1}{2Q}, \quad Q = k\,|H(\omega_n)|\]

Half-Power Bandwidth:

\[\zeta = \frac{\Delta f}{2f_n} = \frac{f_2 - f_1}{2f_n}\]

Where \(f_1, f_2\) are half-power points (\(|H| = |H_{max}|/\sqrt{2}\))

Circle Fit (Nyquist Plot):

For well-separated modes, FRF traces a circle in Nyquist plot (Real vs Imaginary). Fitting circle provides:

Rational Fraction Polynomial (Advanced):

\[H(\omega) = \frac{b_0 + b_1(j\omega) + \cdots + b_m(j\omega)^m}{a_0 + a_1(j\omega) + \cdots + a_n(j\omega)^n}\]

Polynomial coefficients solved from measured data; poles yield natural frequencies and damping

Complex Mode Indicator Function (CMIF):

Uses SVD of FRF matrix to identify number of modes and separate closely spaced modes

Mode Extraction Settings

40
3.0
2

Extraction Method:

Extracted Parameters:

True Frequency: 40.0 Hz

Extracted Frequency: -- Hz

Frequency Error: -- %

True Damping: 3.0 %

Extracted Damping: -- %

Damping Error: -- %

Data Quality and Coherence

Coherence Function

The coherence function quantifies the quality of FRF measurement by indicating how much of the output is linearly related to the input. Values near 1.0 indicate good measurements; values significantly below 1.0 suggest problems.

Coherence Definition:

\[\gamma^2(\omega) = \frac{|G_{XF}(\omega)|^2}{G_{XX}(\omega)G_{FF}(\omega)}\]

Where:

Causes of Poor Coherence:

Improving Coherence:

Measurement Quality

40
10

Measurement Issues:

Data Quality Assessment

Avg coherence: 0.00  |  Min: 0.00  |  Quality: Excellent

γ²>0.95 Excellent  ·  0.90–0.95 Good  ·  0.80–0.90 Fair  ·  <0.80 Poor

Engineering Applications

Modal testing and experimental modal analysis are everyday tools in several industries:

Summary of Key Equations

Concept Equation Description
FRF Definition \(H(\omega) = \frac{X(\omega)}{F(\omega)}\) Ratio of response to force in frequency domain
SDOF Receptance \(H(\omega) = \frac{1/k}{1 - r^2 + j(2\zeta r)}\) Single degree of freedom FRF
Modal Superposition \(H_{jk}(\omega) = \sum_{r=1}^{N} \frac{\Phi_{jr}\Phi_{kr}}{m_r(\omega_{r}^2 - \omega^2 + j2\zeta_r\omega_r\omega)}\) Multi-mode FRF summation
Half-Power Damping \(\zeta = \frac{\Delta f}{2f_n}\) Damping from bandwidth at peak/√2
Coherence \(\gamma^2(\omega) = \frac{|G_{XF}(\omega)|^2}{G_{XX}(\omega)G_{FF}(\omega)}\) Measurement quality indicator (0 to 1)

Practice Problems

Problem 1: Half-Power Bandwidth Method

An FRF shows a resonance peak at 45 Hz with magnitude 0.005 m/N. The half-power points occur at 43.5 Hz and 46.5 Hz. Calculate the damping ratio.

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Problem 2: Modal Mass Calculation

An FRF peak at 30 Hz has a receptance magnitude of 0.01 m/N. Given that \(\zeta = 2\%\), calculate the modal mass assuming the measurement was at maximum mode shape location (\(\Phi = 1\)).

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Problem 3: Required Averages for Coherence

A measurement shows coherence of 0.85 with 5 averages. Approximately how many averages are needed to achieve coherence of 0.95, assuming random noise is the limiting factor?

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Knowledge Check Quiz

Question 1: What does the FRF represent?

Question 2: Which FRF type is measured as acceleration/force?

Question 3: The half-power bandwidth method determines:

Question 4: Coherence values close to 1.0 indicate:

Question 5: Impact testing is most suitable for: