Numerical simulation of the tip aerodynamics and acoustics test

Author:

Tejero E F.,Doerffer P.,Szulc O.,Cross J. L.

Publisher

Springer Science and Business Media LLC

Subject

Condensed Matter Physics

Reference18 articles.

1. Cross J.L. and Watts M.E.: Tip aerodynamics and acoustics test, NASA Reference Publication 1179, 1988

2. Hernandez F. and Johnson W.: Correlation of airloads on a two-bladed helicopter rotor, International Specialist Meeting on Rotorcraft Acoustics and Rotor Fluid Dynamics, 1991, Philadelphia (United States)

3. Ramachandran K., Schlechtriem S., Caradonna F.X. and Steinhoff J.S.: Free-wake computation of helicopter rotor flowfield in forward flight, AIAA Paper 93–3079, Reno, NV,USA, 1993

4. Ahmad J. and Duque P.N.: Helicopter rotor blade computation in unsteady flows using moving overset grids, Journal of Aircraft, vol. 33, no. 1, 1996, pp. 54–60

5. Jung M.S. and Kwon O.J.: Numerical simulation of unsteady rotor flow using an unstructured overset mesh flow solver, Int. Journal of Aeronautical & Space Sciences, vol. 10, no. 1, 2009, pp. 104–111

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