Analysis of Aeroacoustic Sources Using Large Eddy Simulation of an Open Fan Blade at Full Scale

Author:

Karve Ravish1,Priebe Stephan1,Jourdan Eduardo1,Mousavi Arash2,Chakrabarti Suryapratim1,D'Aquila Luke1,Yi Junsok1,Alhawwary Mohammad1,Bharadwaj Ananthan Varun2,Ramakrishnan Kishore1,Wood Trevor H.1

Affiliation:

1. General Electric Company Research

2. GE Aerospace

Publisher

American Institute of Aeronautics and Astronautics

Reference32 articles.

1. Khalid, S. A., Lurie, D., Breeze-Stringfellow, A., Wood, T., Ramakrishnan, K., Paliath, U., Wojno, J., Janardan, B., Goerig, T., and Opalski, A. "Open rotor engine aeroacoustic technology," Final Report DOT/FAA/AEE/2014-04, FAA Continuous Lower Energy, Emissions and Noise (CLEEN) Program,2013. URLhttps://www.faa.gov/sites/faa.gov/files/about/ office_org/headquarters_offices/apl/Open_Rotor_Public_Final_Report.pdf.

2. Progress in open rotor propulsors: The FAA/GE/NASA open rotor test campaign

3. Computational Aerodynamics Development and Outlook

4. Grid-point requirements for large eddy simulation: Chapman’s estimates revisited

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