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2018 | OriginalPaper | Chapter

8. Dynamic Response of Shell Structures to Random Acoustic Excitation, SDOF Approximation

Author : Jaap Wijker

Published in: Miles' Equation in Random Vibrations

Publisher: Springer International Publishing

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Abstract

Three approximate methods to calculate the responses of shell structures when exposed to an acoustic pressure field using a single degree of freedom (SDOF) system approach are discussed in this chapter. The most straightforward method is the approximation applying the second approach, when the acoustic pressure field is proportional to the assumed or vibration mode of the shell structure. To gain more insight examples and problems with answers are provided.

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previous chapter Preliminary Predictions of Loads Induced by Acoustic Environment
next chapter Equivalence Random and Sinusoidal Vibration
Appendix
Available only for authorised users
Literature
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Cunningham PR, Langley RS, White RG (2003) Dynamic response of doubly curved honeycomb sandwich panels to random acoustic excitation, part 2: theoretical study. J Sound Vib 264:605–637CrossRef
2.
Prescott J (1961) Applied elasticity. Dover Publications Inc. New York
3.
Meirovitch L (1980) Computational methods in structural dynamics. Sijthoff and Noordhoff. ISBN 90 286 05800
4.
Temple G, Bickley WG (1956) Rayleigh’s principle and applications to engineering. Dover Publications, New York
5.
Blevins RD (1995) Formulas for natural frequency and mode shape. Krieger Publishing Company. ISBN 0-89464-894-2
6.
Dhainaut JM, Cheng G, Mei C (2014) Response of plates under statistically unsynchronized uniform random loads using monte-carlo simulation. J Comput Appl Mech 9(1):3–18MathSciNetMATH
7.
Johns DJ, Nagaraj VT (1968) On the fundatmental frequency of square plate symmetrically supported at four points. J Sound Vib 10(3):404–410CrossRefMATH
8.
Metadata
Title
Dynamic Response of Shell Structures to Random Acoustic Excitation, SDOF Approximation
Author
Jaap Wijker
Copyright Year
2018
Book
Miles' Equation in Random Vibrations

Print ISBN: 978-3-319-73113-1

Electronic ISBN: 978-3-319-73114-8

Copyright Year: 2018

DOI
https://doi.org/10.1007/978-3-319-73114-8_8

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