Abstract
The good agreement of the numerical results with experiments in both hover and forward flight indicates the accuracy and suitability of the TURNS code for helicopter aerodynamics and acoustics simulations.
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Srinivasan, G.R. (1995). Advances in Euler and Navier-Stokes methods for helicopter applications. In: Deshpande, S.M., Desai, S.S., Narasimha, R. (eds) Fourteenth International Conference on Numerical Methods in Fluid Dynamics. Lecture Notes in Physics, vol 453. Springer, Berlin, Heidelberg. https://doi.org/10.1007/3-540-59280-6_184
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DOI: https://doi.org/10.1007/3-540-59280-6_184
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