Reduction of rotorcraft BVI using synthetic jets; computational studies using LES
Author:
Affiliation:
1. Department of Mechanical Engineering, Georgia Southern University, Statesboro, Georgia, USA
Publisher
Informa UK Limited
Link
https://www.tandfonline.com/doi/pdf/10.1080/15502287.2023.2291009
Reference56 articles.
1. Rotorcraft BVI noise reduction by attitude modification
2. Wake Displacement Study of Attitude and Flight Parameter Modifications to Reduce Rotorcraft Blade-Vortex Interaction (BVI) Noise
3. F. X. Caradonna C. Kitaplioglu and M. McCluer “An experimental study of parallel blade–vortex interaction aerodynamics and acoustics utilizing an independently generated vortex ” NASA Ames Research Center TM 199208790 Moffett Field CA 1999.
4. Examination of vortex deformation during blade-vortex interaction
5. Calculation of blade-vortex interaction airloads on helicopter rotors
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