Geodesic
Numerical simulation of gas flows around aircraft with allowance for the flow/exhaust jet interaction
Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki, Tome 55 (2015) no. 4, pp. 681-694

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Three-dimensional steady gas flow around aircraft in the presence of an exhaust jet are considered. The mathematical flow model is based on the Reynolds-averaged Navier–Stokes equations for a two-component equilibrium turbulent medium and a two-parameter semiempirical turbulence model. A numerical implementation of the model is described. Numerical examples are given. 
@article{ZVMMF_2015_55_4_a14,
     author = {D. A. Zabarko and V. I. Zubov and V. P. Kotenev and V. M. Krivtsov and Yu. A. Polezhaev},
     title = {Numerical simulation of gas flows around aircraft with allowance for the flow/exhaust jet interaction},
     journal = {\v{Z}urnal vy\v{c}islitelʹnoj matematiki i matemati\v{c}eskoj fiziki},
     pages = {681--694},
     publisher = {mathdoc},
     volume = {55},
     number = {4},
     year = {2015},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/ZVMMF_2015_55_4_a14/}
}
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D. A. Zabarko; V. I. Zubov; V. P. Kotenev; V. M. Krivtsov; Yu. A. Polezhaev. Numerical simulation of gas flows around aircraft with allowance for the flow/exhaust jet interaction. Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki, Tome 55 (2015) no. 4, pp. 681-694. http://geodesic.mathdoc.fr/item/ZVMMF_2015_55_4_a14/