Numerical Simulation of Blade Vortex Interaction (BVI) In Helicopter Using Large Eddy Simulation (LES) Method

Author:

Syriac John Sherjy,Vinod Narayanan

Publisher

Springer Singapore

Reference13 articles.

1. Khier W Numerical simulation of a complete helicopter configuration in forward flight using fluid-structure coupling. Springer Publishing, New Results in Numerical and Experimental Fluid

2. Yu YH (2000) Rotor blade-vortex interaction noise. Progress in Aerospaces Sciences 36(2) (2000)

3. Boxwell DA, Splettstoesser WR, Schultz KJ, Schmitz FH (1987) Helicopter model rotor-blade vortex interaction impulsive noise: scalability and parametric variations. J Am Helicopt Soc 32(1):3–12

4. Zioutis XK, Spyropoulos AI, Margaris DP, Papanikas DG (2004) Numerical investigation of BVI modeling effects on helicopter rotor free wake simulations. International Congress of the Aeronautical Sciences, ICAS-2004

5. Lowson MV (1991) Progress towards quieter civil helicopters. 17th European Rotorcraft Forum, Berlin, September 1991

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