Abstract The results of experimental laboratory studies of an acoustic field inside the stiffened shell are presented; the shell simulates an aircraft fuselage compartment under its excitation by a diffusion sound field. The soundproofing capacity of the model compartment under diffusion excitation is experimentally evaluated.
Determination of a soundproofing capacity of the model aircraft fuselage compartment
Russian Aeronautics (Iz VUZ) ; 52 , 2 ; 235-239
2009-06-01
5 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Determination of a soundproofing capacity of the model aircraft fuselage compartment
Online Contents | 2009
|FUSELAGE COMPARTMENT OF THE AIRCRAFT WITH A HATCH CUTOUT
Europäisches Patentamt | 2018
|Aircraft having self-erecting partition element in compartment inside fuselage
Europäisches Patentamt | 2015
|MULTILAYER PANEL FOR SOUNDPROOFING AIRCRAFT INTERIORS
Europäisches Patentamt | 2023
|