Matematičeskoe modelirovanie, Tome 11 (1999) no. 4, pp. 19-28
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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/
@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
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.
