Validation of a Moving-Body High-Order Immersed Boundary Method for the Multiple Pure Tone Noise Generated by Supersonic Rotor Cascades (AIAA 2015-2518)
Aeroacoustics ; 2015 ; Dallas, TX
01.01.2015
18 pages
Aufsatz (Konferenz)
Englisch
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GPU Parallelization of a High Order Immersed Boundary Method Fluid Solver (AIAA 2015-3056)
British Library Conference Proceedings | 2015
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