Influence of Blade Deformations on Open-Rotor Low-Speed and High-Speed Aerodynamics and Aeroacoustics

Author:

Falissard F.,Boisard R.,Gaveriaux R.,Delattre G.,Gardarein P.,Chelius A.,Canard-Caruana S.,Mauffrey Y.

Funder

Horizon 2020 Framework Programme

FP7 Joint Technology Initiatives

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference39 articles.

1. Airbus AI-PX7 CROR Design Features and Aerodynamics

2. KhalidS.LurieD.Breeze-StringfellowA.WoodT.RamakrishnanK.PaliathU.WojnoJ.JanardanB.GoerigT.OpalskiA.et al. “Open Rotor Engine Aeroacoustic Technology CLEEN Project Final Report,” GE Aviation Tech. Rept. DOT/FAA/AEE/2014-04, Cincinnati, OH, 2013.

3. Application of an efficient hybrid scheme for aeroelastic analysis of advanced propellers

4. Structural and aerodynamic analysis of a large-scale advanced propeller blade

5. High-speed propeller noise prediction - A multidisciplinary approach

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