Theory and Design for Mechanical Measurements
Theory and Design for Mechanical Measurements
6th Edition
ISBN: 9781118881279
Author: Richard S. Figliola, Donald E. Beasley
Publisher: WILEY
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Chapter 2, Problem 2.32P

A particular strain sensor is mounted to an aircraft wing that is subjected to periodic wind gusts. The strain measurement system indicates a periodic strain that ranges from 3250 x 10 6 in./in. to 4150 x 10-6 inJin. at a frequency of 1 Hz.

  1. Determine the average value of this signal.
  2. Determine the amplitude and the frequency of this output signal when expressed as a simple periodic function.
  3. Determine a one-term Fourier series that represents this signal.
  4. Construct an amplitude spectrum plot for the output signal.

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0.36 If the mass and the stiffness matrix of the obtained equation is given by M = 0.36 [50.884 K = -45 50.884 -45 Determine: 1.4 the normalized stiffness K; 1.5 the natural frequencies of the system in Hz for the value considered above; 1.6 its eigenvalues and eigenvectors and hence; and 1.7 the modal matrix P and the diagonalised spectral matrix A.
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Theory and Design for Mechanical Measurements

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