Abstract
The time resolved flow and acoustic fields around a simplified two-wheel nose landing gear configuration featuring brakes, torque link, and a detachable fairing are investigated by numerical and experimental means. The flow field is computed by a lattice Boltzmann method with a collision step based on countable cumulants. Numerical near field flow predictions are validated by experimental results from Delft University of Technology. The comparison shows the quality of the applied computational setup and methodology. The favorable noise mitigation properties of the installed fairing are discussed.
Original language | English |
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Title of host publication | 28th AIAA/CEAS Aeroacoustics 2022 Conference |
Number of pages | 10 |
ISBN (Electronic) | 978-1-62410-664-4 |
DOIs | |
Publication status | Published - 2022 |
Event | 28th AIAA/CEAS Aeroacoustics 2022 Conference - Southampton, United Kingdom Duration: 14 Jun 2022 → 17 Jun 2022 Conference number: 28 |
Publication series
Name | 28th AIAA/CEAS Aeroacoustics Conference, 2022 |
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Conference
Conference | 28th AIAA/CEAS Aeroacoustics 2022 Conference |
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Country/Territory | United Kingdom |
City | Southampton |
Period | 14/06/22 → 17/06/22 |