Effect of the bulkhead fixing on the noise inside the airplane cabin

Auteurs-es

  • L. Cheng Dept. of Mech. Eng., Sherbrooke Univ., Que., Canada
  • J. Nicols Dept. of Mech. Eng., Sherbrooke Univ., Que., Canada

Mots-clés :

aircraft, architectural acoustics, noise abatement, cabin noise, airplanes, Challenger 601-3A, fixing conditions, rear-pressure bulkhead

Résumé

This work describes one step of a research program undertaken by the authors to investigate the cabin noise of airplanes (more specifically the Challenger 601-3A made by Canadair). It focuses on the effect of the fixing conditions of the rear-pressure bulkhead on the internal cabin noise. The idealized model simulating the problem is the radiation of sound from point-driven circular plates into a hard-walled cylindrical enclosure

Fichiers supplémentaires

Publié-e

1991-09-01

Comment citer

1.
Cheng L, Nicols J. Effect of the bulkhead fixing on the noise inside the airplane cabin. Canadian Acoustics [Internet]. 1 sept. 1991 [cité 15 mai 2026];19(4):11-2. Disponible à: https://jcaa.caa-aca.ca/index.php/jcaa/article/view/645

Numéro

Vol. 19 No. 4 (1991)

Rubrique

Actes du congrès de la Semaine canadienne d'acoustique

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