Aerodynamic and Aero-acoustic Analysis of Helicopter Rotor Blades in Hover

Author:

Doerffer Piotr,Szulc Oskar,Embuena Fernando Tejero,Suarez Javier Martinez

Publisher

Springer International Publishing

Reference21 articles.

1. Caradonna, F.X., Tung, C.: Experimental and analytical studies of a model helicopter rotor in hover. NASA Technical Memorandum, 81232 (1981)

2. Kang, H.J., Kwon, O.J.: Unstructured mesh Navier-Stokes calculations of the flow field of a helicopter rotor in hover. J. of the American Helicopter Society 47(2), 90–99 (2002)

3. Sun, H., Lee, S.: Response surface approach to aerodynamic optimization design of helicopter rotor blade. J. Numer. Meth. Engng. 64, 125–142 (2005)

4. Song, W.P., Han, Z.H., Qiao, Z.D.: Computational aeroacoustic prediction of transonic rotor noise based on Reynolds-Averaged Navier-Stokes flow simulation. In: 25th Congress of the International Council of the Aeronautical Sciences, Paper ICAS 2006-2.10.3, Hamburg (2006)

5. Xu, J.H., Song, W.P., Xie, F.T.: Application of high-resolution scheme in rotor flow simulation. In: 27th Congress of the International Council of the Aeronautical Sciences, Paper ICAS 2010-2.1.3, Nice (2010)

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