Increasingly demanding community noise targets are promoting noise performance ever higher on the list of airliner design drivers. In response, significant noise reductions are being made, though at a declining rate - it appears that a whole airframe approach is now needed to achieve significant further gains. As a possible step in this direction, over-wing engine installations are considered here, which use the airframe itself as a noise shield. The paper is the account of an experimental investigation of the comparative shielding performances of a range of relative engine positions on such a layout Using the statistical modelling technique Kriging, we build an approximation of the noise shielding metric as a function of the position of the engines above the wing - this can serve as the input to multi-disciplinary design trade-off studies. We then compare the results found with the results of applying simple half-barrier diffraction theory to the same problem. We conclude that the latter could be considered as a first order, conceptual design tool, though it misses certain features of the design merit landscape identified by the experiment presented here.
Fan broadband noise shielding for over-wing engines
Breitbandige Lärmabschirmung des Fans bei Triebwerken über dem Flügel
Journal of Sound and Vibration ; 331 , 23 ; 5054-5068
2012
15 Seiten, 20 Bilder, 21 Quellen
Aufsatz (Zeitschrift)
Englisch
Fan broadband noise shielding for over-wing engines
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