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Random Vibrations Simplified Response Analysis

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Spacecraft Structures
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Abstract

Simplified approximate analysis procedures are provided to calculate the random response characteristics of deterministic structures exposed to random mechanical and acoustic loads. Many examples are presented to illustrate the theory.

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© 2008 Springer-Verlag Berlin Heidelberg

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(2008). Random Vibrations Simplified Response Analysis. In: Spacecraft Structures. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-75553-1_21

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  • DOI: https://doi.org/10.1007/978-3-540-75553-1_21

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-540-75552-4

  • Online ISBN: 978-3-540-75553-1

  • eBook Packages: EngineeringEngineering (R0)

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