Tuned mass dampers for flight vehicle components subjected to rocket noise

Jain, P.; Mukherjee, Abhijit; Krishna, Y.

doi:10.1016/j.ast.2010.11.004

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Authors

Jain, P.

Mukherjee, Abhijit

Krishna, Y.

Date

2011

Type

Journal Article

Metadata

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Citation

Jain, P. and Mukherjee, A. and Krishna, Y. 2011. Tuned mass dampers for flight vehicle components subjected to rocket noise. Aerospace Science and Technology. 15 (3): pp. 175-182.

Source Title

Aerospace Science and Technology

DOI

10.1016/j.ast.2010.11.004

ISSN

1270-9638

School

Office of Research and Development

URI

http://hdl.handle.net/20.500.11937/18360

Collection

Curtin Research Publications

Abstract

In this study, response of a flight vehicle component to rocket noise is considered. Tuned mass dampers, hitherto used in low frequency excitation, have been utilized to attenuate high frequency, broad band excitations. Modally tuned dampers have been investigated for a variety of input excitations. Modal dampers exhibit significant attenuation of all input signals. © 2010 Elsevier Masson SAS.