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Nonlinear Vibrations of Aerospace Structures · NNM (Nonlinear Normal Modes) continuation Global...

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Nonlinear normal modes Frequency-energy plot T04 Nonlinear modal analysis Nonlinear Vibrations of Aerospace Structures
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Page 1: Nonlinear Vibrations of Aerospace Structures · NNM (Nonlinear Normal Modes) continuation Global analysis mode 1: 310631 Hz Measure Identify Model Simulate Understand Design Use .

Nonlinear normal modes

Frequency-energy plot

T04 Nonlinear modal analysis

Nonlinear Vibrations of

Aerospace Structures

Page 2: Nonlinear Vibrations of Aerospace Structures · NNM (Nonlinear Normal Modes) continuation Global analysis mode 1: 310631 Hz Measure Identify Model Simulate Understand Design Use .

Tutorial 1: The First Mode of

the Nonlinear Beam

Page 3: Nonlinear Vibrations of Aerospace Structures · NNM (Nonlinear Normal Modes) continuation Global analysis mode 1: 310631 Hz Measure Identify Model Simulate Understand Design Use .

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2.37.109 𝑥3

0.289𝑥 + 0.1357𝑥 + 11009𝑥 = 𝐹𝑠𝑖𝑛𝜔𝑡

Linear model identified at low level (31 Hz, 0.12%):

Nonlinearity identified at high level:

The Nonlinear Beam

Page 4: Nonlinear Vibrations of Aerospace Structures · NNM (Nonlinear Normal Modes) continuation Global analysis mode 1: 310631 Hz Measure Identify Model Simulate Understand Design Use .

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The Nonlinear Beam

No forcing, no damping

Page 5: Nonlinear Vibrations of Aerospace Structures · NNM (Nonlinear Normal Modes) continuation Global analysis mode 1: 310631 Hz Measure Identify Model Simulate Understand Design Use .

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The NNM Solver

Page 6: Nonlinear Vibrations of Aerospace Structures · NNM (Nonlinear Normal Modes) continuation Global analysis mode 1: 310631 Hz Measure Identify Model Simulate Understand Design Use .

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Set Appropriate Parameters

Page 7: Nonlinear Vibrations of Aerospace Structures · NNM (Nonlinear Normal Modes) continuation Global analysis mode 1: 310631 Hz Measure Identify Model Simulate Understand Design Use .

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Compute The First Nonlinear Mode

Page 8: Nonlinear Vibrations of Aerospace Structures · NNM (Nonlinear Normal Modes) continuation Global analysis mode 1: 310631 Hz Measure Identify Model Simulate Understand Design Use .

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30 35 400

0.01

0.02

0.03

0.04

The Link Between Nonlinear Modes and FRFs

8 8

Frequency (Hz)

x

(m)

10-4

10-1

30

40

50

Energy (J)

Resonance

frequency (Hz)

Backbone

Nonlinear

FRFs

Nonlinear

modes

Page 9: Nonlinear Vibrations of Aerospace Structures · NNM (Nonlinear Normal Modes) continuation Global analysis mode 1: 310631 Hz Measure Identify Model Simulate Understand Design Use .

Tutorial 2: The Modes of a

Multi-DOF System

Page 10: Nonlinear Vibrations of Aerospace Structures · NNM (Nonlinear Normal Modes) continuation Global analysis mode 1: 310631 Hz Measure Identify Model Simulate Understand Design Use .

10

Create a 2-DOF Model

2

0

Page 11: Nonlinear Vibrations of Aerospace Structures · NNM (Nonlinear Normal Modes) continuation Global analysis mode 1: 310631 Hz Measure Identify Model Simulate Understand Design Use .

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Modify the 2-DOF Model

7

Introduce a

linear spring

Page 12: Nonlinear Vibrations of Aerospace Structures · NNM (Nonlinear Normal Modes) continuation Global analysis mode 1: 310631 Hz Measure Identify Model Simulate Understand Design Use .

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The Final Model

Page 13: Nonlinear Vibrations of Aerospace Structures · NNM (Nonlinear Normal Modes) continuation Global analysis mode 1: 310631 Hz Measure Identify Model Simulate Understand Design Use .

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In-Phase Mode: Set Appropriate Parameters

13

Page 14: Nonlinear Vibrations of Aerospace Structures · NNM (Nonlinear Normal Modes) continuation Global analysis mode 1: 310631 Hz Measure Identify Model Simulate Understand Design Use .

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In-Phase Mode: The Resonance Frequencies

Page 15: Nonlinear Vibrations of Aerospace Structures · NNM (Nonlinear Normal Modes) continuation Global analysis mode 1: 310631 Hz Measure Identify Model Simulate Understand Design Use .

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In-Phase Mode: The Modal Shapes

CTRL + LEFT CLICK

Page 16: Nonlinear Vibrations of Aerospace Structures · NNM (Nonlinear Normal Modes) continuation Global analysis mode 1: 310631 Hz Measure Identify Model Simulate Understand Design Use .

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In-Phase Mode: The Time Series

Double click + A

Page 17: Nonlinear Vibrations of Aerospace Structures · NNM (Nonlinear Normal Modes) continuation Global analysis mode 1: 310631 Hz Measure Identify Model Simulate Understand Design Use .

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In-Phase Mode: Harmonics

Double click + A

Page 18: Nonlinear Vibrations of Aerospace Structures · NNM (Nonlinear Normal Modes) continuation Global analysis mode 1: 310631 Hz Measure Identify Model Simulate Understand Design Use .

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Out-of-Phase Mode: Set the Parameters

Right click

Page 19: Nonlinear Vibrations of Aerospace Structures · NNM (Nonlinear Normal Modes) continuation Global analysis mode 1: 310631 Hz Measure Identify Model Simulate Understand Design Use .

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Out-of-Phase Mode: Frequencies and Modal Shapes

Page 20: Nonlinear Vibrations of Aerospace Structures · NNM (Nonlinear Normal Modes) continuation Global analysis mode 1: 310631 Hz Measure Identify Model Simulate Understand Design Use .

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Let’s Go Back to the In-Phase Mode

Right click

Page 21: Nonlinear Vibrations of Aerospace Structures · NNM (Nonlinear Normal Modes) continuation Global analysis mode 1: 310631 Hz Measure Identify Model Simulate Understand Design Use .

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Two New Features

?

?


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