Description

Book Synopsis
Enables engineers to understand the most important aspects of rotating machine vibrations, from basic explanations to more accurate numerical models and analysis. This book, together with the the associated MATLAB software, will give engineers the confidence to base their designs on calculations and understand any dynamic phenomena that might occur.

Table of Contents
1. Introduction; 2. Introduction to vibration analysis; 3. Free lateral response of simple rotor models; 4. Finite element modeling; 5. Free lateral response of complex systems; 6. Forced lateral response and critical speeds; 7. Asymmetric rotors and other sources of instability; 8. Balancing; 9. Axial and torsional vibration; 10. More complex rotordynamic models.

Dynamics of Rotating Machines 26 Cambridge Aerospace Series Series Number 28

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    A Hardback by Arthur W. Lees, John E. T. Penny, Seamus D. Garvey

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      View other formats and editions of Dynamics of Rotating Machines 26 Cambridge Aerospace Series Series Number 28 by Arthur W. Lees

      Publisher: Cambridge University Press
      Publication Date: 3/31/2010 12:00:00 AM
      ISBN13: 9780521850162, 978-0521850162
      ISBN10: 0521850169
      Also in:
      Thermodynamics and heat Aerospace and aviation technology

      Description

      Book Synopsis
      Enables engineers to understand the most important aspects of rotating machine vibrations, from basic explanations to more accurate numerical models and analysis. This book, together with the the associated MATLAB software, will give engineers the confidence to base their designs on calculations and understand any dynamic phenomena that might occur.

      Table of Contents
      1. Introduction; 2. Introduction to vibration analysis; 3. Free lateral response of simple rotor models; 4. Finite element modeling; 5. Free lateral response of complex systems; 6. Forced lateral response and critical speeds; 7. Asymmetric rotors and other sources of instability; 8. Balancing; 9. Axial and torsional vibration; 10. More complex rotordynamic models.

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