Jet-wing interaction: computational modelling based on MILES CABARET and acoustic analogy
Author:
Affiliation:
1. Queen Mary, University of London
2. Central Aerohydrodynamic Institute
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-2475
Reference13 articles.
1. 1Kopiev, V.F., Faranosov, G.A., Zaytsev, M.Yu., Vlasov, E.V., Karavosov, R.K., Belyaev, I.V., Ostrikov, N.N. "Intensification and suppression of jet noise sources in the vicinity of lifting surfaces," AIAA 2013-2284
2. Compact Accurately Boundary-Adjusting high-REsolution Technique for fluid dynamics
3. CABARET method on unstructured hexahedral grids for jet noise computation
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1. CABARET GPU Solver for Fast-Turn-Around Flow and Noise Calculations;21st AIAA/CEAS Aeroacoustics Conference;2015-06-18
2. Empiricism-free noise calculation from LES solution based on Goldstein generalized acoustic analogy: volume noise sources and meanflow effects;21st AIAA/CEAS Aeroacoustics Conference;2015-06-18
3. Computational modelling of jet-wing interaction: the effect of asymmetries from the jet inflow conditions and the wing;21st AIAA/CEAS Aeroacoustics Conference;2015-06-18
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