Open AccessPrediction of Turbulent Boundary Layer Induced Noise in the Cabin of a BWB Aircraft
Author(s) -
Joana Rocha,
Afzal Suleman,
Fernando Lau
Publication year - 2012
Publication title -
shock and vibration
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.418
H-Index - 45
eISSN - 1875-9203
pISSN - 1070-9622
DOI - 10.1155/2012/153204
Subject(s) - boundary layer , turbulence , noise (video) , range (aeronautics) , acoustics , aircraft noise , sound pressure , volume (thermodynamics) , flow (mathematics) , boundary (topology) , aerospace engineering , engineering , mechanics , physics , computer science , mathematics , noise reduction , mathematical analysis , quantum mechanics , artificial intelligence , image (mathematics)
This paper discusses the development of analytical models for the prediction of aircraft cabin noise induced by the external turbulent boundary layer (TBL). While, in previous works, the contribution of an individual panel to the cabin interior noise was considered, here, the simultaneous contribution of multiple flow-excited panels is analyzed. Analytical predictions are presented for the interior sound pressure level (SPL) at different locations inside the cabin of a Blended Wing Body (BWB) aircraft, for the frequency range 0–1000 Hz. The results show that the number of vibrating panels significantly affects the interior noise levels. It is shown that the average SPL, over the cabin volume, increases with the number of vibrating panels. Additionally, the model is able to predict local SPL values, at specific locations in the cabin, which are also affected with by number of vibrating panels, and are different from the average values.