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},
year = {1999},
volume = {11},
number = {4},
language = {ru},
url = {http://geodesic.mathdoc.fr/item/MM_1999_11_4_a2/}
}
TY - JOUR AU - S. B. Svirschevsky AU - N. V. Semenchikov AU - N. V. Korolev TI - Research of aerodynamics of missile afterbody with ring nozzle in trans- and supersonic stream JO - Matematičeskoe modelirovanie PY - 1999 SP - 19 EP - 28 VL - 11 IS - 4 UR - http://geodesic.mathdoc.fr/item/MM_1999_11_4_a2/ LA - ru ID - MM_1999_11_4_a2 ER -
%0 Journal Article %A S. B. Svirschevsky %A N. V. Semenchikov %A N. V. Korolev %T Research of aerodynamics of missile afterbody with ring nozzle in trans- and supersonic stream %J Matematičeskoe modelirovanie %D 1999 %P 19-28 %V 11 %N 4 %U http://geodesic.mathdoc.fr/item/MM_1999_11_4_a2/ %G ru %F MM_1999_11_4_a2
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/