Scaling procedures of cabin noise generated by turbulent boundary layer excitation

Author:

ZHAO Xiaojian,SONG Wei,ZHOU Jie,AI Bangcheng

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference26 articles.

1. Corcos GM, Liepmann HW. On the contribution of turbulent boundary layers to the noise inside a fuselage. Washington, D.C.:NACA;1956. Report No.: NACA-TM-1420.

2. Alex LJS. Airplane interior noise modeling using Statistical Energy Analysis Approach. Reston:AIAA;1999. Report No.: AIAA-1999-1903.

3. Joakim H. SAAB’S experience in aircraft interior noise and vibration measurements. Reston:AIAA;1999. Report No.: AIAA-1999-1837.

4. Francesco M, Antonia S, Marco A. Interior noise sources identifications, in-flight measurements and numerical correlations of an advanced business aircraft. Reston:AIAA;2006. Report No.: AIAA-2006-2491.

5. Blakemore M, Heron KH, Davis EB. A new wavenumber-based approach for predicting aircraft cabin noise. Reston:AIAA;2008. Report No.: AIAA-2008-3009.

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