The use of spatial coherence techniques for identifying noise transmission paths on the MDC-UHB demonstrator aircraft

Application of partial coherence techniques to determination of the transmission paths of sound into an airplane cabin interior has been studied. Accurate quantitative information on the dominant paths of acoustic energy transmission can be obtained with this technique as well as the relative contributions from airborne and structure-borne paths. This information is useful in making design changes in the fuselage to reduce the interior cabin noise. The techniques are successfully applied to noise and vibration data collected during flight tests of the McDonnel Douglas Ultra-High Bypass Demonstrator aircraft, and these results are compared with other data measured during the flight program.