The response of a supersonic transport fuselage to boundary layer and to reverberant noise
- 31 January 1969
- journal article
- Published by Elsevier in Journal of Sound and Vibration
- Vol. 9 (1) , 6-20
- https://doi.org/10.1016/0022-460x(69)90258-2
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Response of a Simply Supported Beam to a Three-Dimensional Reverberant Acoustic FieldThe Journal of the Acoustical Society of America, 1967
- Measurement and analysis of the response field of turbulent boundary layer excited panelsJournal of Sound and Vibration, 1965
- Problems of cabin noise estimation for supersonic transportsJournal of Sound and Vibration, 1964
- The fluctuating pressure field in a supersonic turbulent boundary layerJournal of Fluid Mechanics, 1963
- Measurements of the fluctuating pressure at the wall beneath a thick turbulent boundary layerJournal of Fluid Mechanics, 1962
- Measurement of Correlation Coefficients in Reverberant Sound FieldsThe Journal of the Acoustical Society of America, 1955