Subject
Computer Science Applications,Mechanical Engineering,General Materials Science,Modeling and Simulation,Civil and Structural Engineering
Reference14 articles.
1. Investigation of parallel blade–vortex interaction at low speed;Seath;J Aircraft,1989
2. Papadakis M, Nizampatnam L, Hoffmann K. Computational investigation of blade vortex interaction noise. In: Proceedings of the 38th aerospace sciences meeting and exhibit, Reno (NV). AIAA paper 99-0231; January 10–13 2000.
3. Abelló JC, George AR. Rotorcraft BVI noise reduction by attitude modification. In: Paper presented at the 5th AIAA/CEAS aeroacoustics conference, Bellevue, Washington; May 10–12 1999.
4. Abello J, George A, Wake displacement study of attitude and flight parameter modifications to reduce rotorcraft blade–vortex interaction (BVI) noise. In: Ninth AIAA/CEAS aeroacoustics conference, Hilton Head, SC; May12–14 2003.
5. Examination of vortex deformation during blade–vortex interaction;Horner;AIAA J,1996
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