Accession Number : AD0435911


Title :   AN EXPERIMENTAL INVESTIGATION OF TURBULENCE-EXCITED PANEL VIBRATION AND NOISE (BOUNDARY-LAYER NOISE)


Corporate Author : ADVISORY GROUP FOR AERONAUTICAL RESEARCH AND DEVELOPMENT PARIS (FRANCE)


Personal Author(s) : Baroudi, M Y el ; Ludwig, G R ; Ribner, H S


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/435911.pdf


Report Date : Apr 1963


Pagination or Media Count : 47


Abstract : A study is made of the flexural motion and noise generated by 11 x 11 in. steel panels flush mounted in the wall of a turbulent flow channel. The mean square exciting pressure fluctuation at the wall, its spectral density, and two- point correlations of the pressure were measured with the use of pinhole microphones. The flexural response of sample panels was studied by correlation techniques. The calculated relief plot of correlation shows qualitative agreement with the experimental results.


Descriptors :   *AIRCRAFT NOISE , DAMPING , TURBULENT BOUNDARY LAYER , CORRELATION TECHNIQUES , AIRCRAFT PANELS , VIBRATION , NOISE


Subject Categories : Acoustics


Distribution Statement : APPROVED FOR PUBLIC RELEASE