[HTML][HTML] Turbomachinery simulation challenges and the future

J Tyacke, NR Vadlamani, W Trojak, R Watson… - Progress in Aerospace …, 2019 - Elsevier
Dramatic changes to aircraft design are on the horizon to meet ambitious efficiency and
emissions targets. This will bring about changes in the role and design of aero-engines …

Slat noise in high-lift systems

Y Zhang, L Cattafesta, K Pascioni… - Progress in Aerospace …, 2024 - Elsevier
This paper reviews several decades' worth of research on the topic of slat noise arising from
high-lift systems of commercial aircraft. A high-lift system is commonly used for providing …

Towards an enhanced protection of attached boundary layers in hybrid RANS/LES methods

S Deck, N Renard - Journal of Computational Physics, 2020 - Elsevier
A robust strategy for the RANS shielding of attached boundary layers in a hybrid RANS/LES
context is presented, addressing two major issues. Firstly, the attached boundary layers …

Investigation of the unsteady flow and noise generation in a slat cove

M Terracol, E Manoha, B Lemoine - Aiaa Journal, 2016 - arc.aiaa.org
This study presents hybrid Reynolds-averaged Navier–Stokes/large-eddy simulations of the
unsteady flow and noise-generation phenomena in the slat cove of a high-lift wing profile …

Large-scale contribution to mean wall shear stress in high-Reynolds-number flat-plate boundary layers up to 13650

S Deck, N Renard, R Laraufie… - Journal of Fluid …, 2014 - cambridge.org
Large-scale contribution to mean wall shear stress in high-Reynolds-number flat-plate boundary
layers up to Reθ =13650 Page 1 J. Fluid Mech. (2014), vol. 743, pp. 202–248. c Cambridge …

Assessment of slat noise predictions for 30P30N high-lift configuration from BANC-III workshop

MM Choudhari, DP Lockard - 21st AIAA/CEAS aeroacoustics …, 2015 - arc.aiaa.org
IRFRAME noise corresponds to the acoustic radiation due to turbulent flow in the vicinity of
airframe components such as high-lift devices and landing gear. The combination of …

Aeroacoustic prediction of a multi-element airfoil using wall-modeled large-eddy simulation

Y Zhang, H Chen, K Wang, M Wang - AIAA Journal, 2017 - arc.aiaa.org
Wall-modeled large-eddy simulation is employed in combination with the Ffowcs Williams–
Hawkings equation to predict and analyze the aeroacoustics of a 30P30N three-element …

High-fidelity simulations of unsteady civil aircraft aerodynamics: stakes and perspectives. Application of zonal detached eddy simulation

S Deck, F Gand, V Brunet… - … Transactions of the …, 2014 - royalsocietypublishing.org
This paper provides an up-to-date survey of the use of zonal detached eddy simulations
(ZDES) for unsteady civil aircraft applications as a reflection on the stakes and perspectives …

A second golden age of aeroacoustics?

SK Lele, JW Nichols - Philosophical Transactions of the …, 2014 - royalsocietypublishing.org
In 1992, Sir James Lighthill foresaw the dawn of a second golden age in aeroacoustics
enabled by computer simulations (Hardin JC, Hussaini MY (eds) 1993 Computational …

Flow dynamics past a 30P30N three-element airfoil using improved delayed detached-eddy simulation

N Ashton, A West, F Mendonça - AIAA Journal, 2016 - arc.aiaa.org
NOISE emissions from commercial aircraft during takeoff and landing are crucial limiting
factors in the expansion of current airports, both in terms of their operating hours and …