Low-Speed Turbofan Aerodynamic and Acoustic Prediction with an Isothermal Lattice Boltzmann Method
Author:
Affiliation:
1. ONERA–Paris Saclay University, F-92322 Châtillon, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060752
Reference24 articles.
1. Aeroacoustic study of a wavy stator leading edge in a realistic fan/OGV stage
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