A Hybrid Lattice-Boltzmann/FH-W Method to Predict Sources and Propagation of Landing Gear Noise
Author:
Affiliation:
1. Exa GmbH
2. Exa Corporation
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-3976
Reference14 articles.
1. Prediction of Aeroacoustic Noise from a Simplified Landing Gear Using a Lattice-Boltzmann-Scheme
2. Computational Aeroacoustic Analysis of Flow Around a Complex Nose Landing Gear Configuration
3. Computational Aeroacoustics Validation and Analysis of a Nose Landing Gear
4. 5Zawaodny, N.S., Liu, F., Yardibi, T., Cattafeta, L.N., Khorrami, M.R., Neuhart, D., and Van de Ven, T. "A Comparative Aeroacoustic Study of a ¼-Scale Gulfstream G550 Aircraft Nose Landing Gear Model," AIAA Paper 2009-3153, May2009.
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