Pressure fluctuations recorded on the surface of the LAGOON#1 Landing Gear. Mach number = 0.23 Re_D= 1.541 x 10 (Reynolds number based on the wheel diameter D = 0.3 m) High-frequency recordings enable accurate spectral analysis and a deep insight into the aerodynamically-generated noise sources.
The simulations are performed using ProLB, a software suite based on the lattice Boltzmann method (www.prolb-cfd.com).
For more details about the simulation, please check the following technical article: http://powersys-solutions.com/pdf/?file=Simulations-of-LAGOON%20landing-gear-noise-using-Lattice-Boltzmann-Solver.pdf&software=ProLB
A. Sengissen, J.-C. Giret, C. Coreixas, and J.-F. Boussuge. Simulations of LAGOON landing gear noise using Lattice Boltzmann solver. In 21st AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2015-2993, Dallas, USA. June 22-26, 2015. The LAGOON (LAnding-Gear nOise database for CAA validatiON) project is supported by Airbus and ONERA.
Would you like to learn more on how to reduce aircraft noise through accurate predictions of landing gear noise?
Read the case study on our distribution partners website : https://powersys-solutions.com/case-study-reducing-aircraft-noise-through-accurate-predictions-of-landing-gear-noise/
More information about ProLB software: http://www.prolb-cfd.com/products/
Try ProLB : https://powersys-solutions.com/contact-us/?service=Trial%20version&software=ProLB