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A finite element method to predict internal noise levels at discrete frequencies for a partially composite helicopter fuselage

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https://hal-upec-upem.archives-ouvertes.fr/hal-00770447
Contributor : Christian Soize <>
Submitted on : Sunday, January 6, 2013 - 1:35:05 PM
Last modification on : Tuesday, March 16, 2021 - 3:42:04 PM

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  • HAL Id : hal-00770447, version 1

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M. Dussac, P. Martin, J. Marze H., F. Chabas, J.-M. David, et al.. A finite element method to predict internal noise levels at discrete frequencies for a partially composite helicopter fuselage. AHS Annual Forum 45, May 1989, Boston, MA, United States. pp.Pages: 1-12. ⟨hal-00770447⟩

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