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Autor:
Jane Meri Santos, Neyval Costa Reis, Gilberto Fisch, Elisa Valentim Goulart, E. G. S. Nascimento, T. T. A. Albuquerque, D. M. Moreira
Publikováno v:
Computational Methods and Experimental Measurements XVII.
This work shows the development of a model for the simulation of rocket exhaust effluent. The model is based on a semi-analytical solution of the time dependent three-dimensional advection-diffusion equation and overcomes the features of the Gaussian