On the Use of the Ffowcs Williams-Hawkings Equation to Predict Far-Field Jet Noise from Large-Eddy Simulations

2013 ◽  
Vol 12 (1-2) ◽  
pp. 1-20 ◽  
Author(s):  
S. Mendez ◽  
M. Shoeybi ◽  
S. K. Lele ◽  
P. Moin
2018 ◽  
Vol 860 ◽  
pp. 1-4 ◽  
Author(s):  
Jonathan B. Freund

Jet noise prediction is notoriously challenging because only subtle features of the flow turbulence radiate sound. The article by Brès et al. (J. Fluid Mech., vol. 851, 2018, pp. 83–124) shows that a well-constructed modelling procedure for the nozzle turbulence can provide unprecedented sub-dB prediction accuracy with modest-scale large-eddy simulations, as confirmed by detailed comparison with turbulence and sound-field measurements. This both illuminates the essential mechanisms of the flow and facilitates prediction for engineering design.


2018 ◽  
Vol 171 ◽  
pp. 166-192 ◽  
Author(s):  
M. Zhu ◽  
C. Pérez Arroyo ◽  
A. Fosso Pouangué ◽  
M. Sanjosé ◽  
S. Moreau

2011 ◽  
Vol 130 (4) ◽  
pp. 2511-2511 ◽  
Author(s):  
Jean-Baptiste Dargaud ◽  
Julien Troyes ◽  
François Vuillot

2020 ◽  
Vol 124 (1275) ◽  
pp. 667-702 ◽  
Author(s):  
S. Unterstrasser ◽  
A. Stephan

AbstractLarge-eddy simulations (LES) have been employed to investigate the far-field four-vortex wake vortex evolution over 10min behind an aircraft formation. In formation flight scenarios, the wake vortex behaviour was found to be much more complex, chaotic and also diverse than in the classical single aircraft case, depending very sensitively on the formation geometry, i.e. the lateral and vertical offset of the two involved aircraft. Even though the case-by-case variability of the wake vortex behaviour across the various formation flight scenarios is large, the final plume dimensions after vortex dissolution are in general substantially different from those of single aircraft scenarios. The plumes are around 170 to 250m deep and 400m to 680m broad, whereas a single A350/B777 aircraft would produce a 480m deep and 330m broad plume. Formation flight plumes are thus not as deep, yet they are broader, as the vortices do not only propagate vertically but also in span-wise direction. Two different LES models have been employed independently and show consistent results suggesting the robustness of the findings. Notably, $CO_{2}$ emissions are only one contribution to the aviation climate impact among several others like contrails and emission of water vapour and nitrogen oxides, which would be all affected by the implementation of formation flight. Thus, we also highlight the differences in ice microphysical and geometrical properties of young formation flight contrails relative to the classical single aircraft case.


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