Browse Topic: Instrument panels
Typical cruising altitudes for business and commercial aircraft are up to 50,000 feet or more. Occupants could not survive in this environment without pressure inside the aircraft being controlled to maintain oxygen concentrations consistent with those at lower altitudes. A cabin pressure warning system typically lets pilots and crews know when pressure becomes dangerously low, but these can malfunction or be accidentally switched off. The result can be insidious and deadly, as those on the plane become slowly incapacitated by hypoxia — oxygen deprivation — without being aware of it.
Three different acoustic finite element models of an automobile passenger compartment are developed and experimentally assessed. The three different models are a traditional model, an improved model, and an optimized model. The traditional model represents the passenger and trunk compartment cavities and the coupling between them through the rear seat cavity. The improved model includes traditional acoustic models of the passenger and trunk compartments, as well as equivalent-acoustic finite element models of the front and rear seats, parcel shelf, door volumes, instrument panel, and trunk wheel well volume. An optimized version of the improved acoustic model is developed by modifying the equivalent-acoustic properties. Modal analysis tests of a vehicle were conducted using loudspeaker excitation to identify the compartment cavity modes and sound pressure response to 500 Hz to assess the accuracy of the acoustic models. The optimized acoustic model is also coupled with a structural
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