Geodesic
Research of aerodynamics of missile afterbody with ring nozzle in trans- and supersonic stream
Matematičeskoe modelirovanie, Tome 11 (1999) no. 4, pp. 19-28.

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The experimental results of the aerodynamic interference of supersonic nonisobaric ring jet with the external streams around a conical afterbody are presented. The flow wave structure of overexpanded and underexpanded jets behind a boat tail has been analyzed. The influence was found of a jet pressure ratio $(N=2.47,\dots, 16.5)$ and freestream Mach number $(M_\infty=0.89,\dots,1.68)$ on the conical afterbody aerodynamic performances. 
@article{MM_1999_11_4_a2,
     author = {S. B. Svirschevsky and N. V. Semenchikov and N. V. Korolev},
     title = {Research of aerodynamics of missile afterbody with ring nozzle in trans- and supersonic stream},
     journal = {Matemati\v{c}eskoe modelirovanie},
     pages = {19--28},
     publisher = {mathdoc},
     volume = {11},
     number = {4},
     year = {1999},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/MM_1999_11_4_a2/}
}
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S. B. Svirschevsky; N. V. Semenchikov; N. V. Korolev. Research of aerodynamics of missile afterbody with ring nozzle in trans- and supersonic stream. Matematičeskoe modelirovanie, Tome 11 (1999) no. 4, pp. 19-28. http://geodesic.mathdoc.fr/item/MM_1999_11_4_a2/