Interior noise radiated by an airplane fuselage subjected to turbulent boundary layer excitation and evaluation of noise reduction treatments-Reference-Cited by-同舟云学术

Interior noise radiated by an airplane fuselage subjected to turbulent boundary layer excitation and evaluation of noise reduction treatments

Published:1971-10 Issue:4 Volume:18 Page:449-464
ISSN:0022-460X
Container-title:Journal of Sound and Vibration
language:en
Short-container-title:Journal of Sound and Vibration

Author:

Bhat W.V.,Wilby J.F.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference11 articles.

1. Measurement of noise radiated by boundary layer excited panels;Maestrello;Journal of Sound and Vibration,1965

2. University of Toronto Institute of Aeronautics Report No. 87;Ludwig;An experimental investigation of the sound generated by thin steel panels excited by turbulent flow,1962

3. Measurements of stiffened cylinder response to turbulent boundary layers;Wilby;U.S. Navy Journal of Underwater Acoustics,1970

4. American Society of Mechanical Engineers Paper No. 70-WA/DE-10;Wilby;Airplane fuselage response to turbulent boundary layers,1970

5. Random noise and vibration in space vehicles;Lyon,1967

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