Geodesic
Selection the first hovering shock wave in the field of gas jet flow
Matematičeskoe modelirovanie, Tome 15 (2003) no. 11, pp. 13-29

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It is given a description of the mathematical model that permits us to build a first hovering shock wave of Laval's nozzle at the expiration of a supersonic jet. This model was worked out within the framework of the structure-element method that orientats us towards creating high-speed software of engineering calculated methods. 
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     author = {E. V. Afanasiev and S. V. Bobyshev and I. L. Dobroserdov},
     title = {Selection the first hovering shock wave in the field of gas jet flow},
     journal = {Matemati\v{c}eskoe modelirovanie},
     pages = {13--29},
     publisher = {mathdoc},
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     number = {11},
     year = {2003},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/MM_2003_15_11_a1/}
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E. V. Afanasiev; S. V. Bobyshev; I. L. Dobroserdov. Selection the first hovering shock wave in the field of gas jet flow. Matematičeskoe modelirovanie, Tome 15 (2003) no. 11, pp. 13-29. http://geodesic.mathdoc.fr/item/MM_2003_15_11_a1/