Some features of viscous gas flow injected into a supersonic stream from the lateral surface of a cylinder

1997 ◽  
Vol 8 (2) ◽  
pp. 154-160
Author(s):  
Z. M. Emel'yanova ◽  
V. M. Paskonov
1967 ◽  
Vol 24 (3) ◽  
pp. 165-166 ◽  
Author(s):  
I.K. Kikoin ◽  
K.I. Balashov ◽  
S.D. Lasarev ◽  
R.E. Neushtadt
Keyword(s):  
Gas Flow ◽  

Author(s):  
Vasily V. Vedeneev

In this paper single mode panel flutter, which occurs at low supersonic Mach numbers, is studied. Numerical analysis which does not require solution of coupled FSI problem has been conducted. Flutter boundaries obtained are compared with previously known analytical results.


AIAA Journal ◽  
2001 ◽  
Vol 39 ◽  
pp. 1313-1319
Author(s):  
R. Padmapriya ◽  
K. P. J. Reddy

2015 ◽  
Vol 10 (3) ◽  
pp. 26-30
Author(s):  
Vladimir Zamuraev ◽  
Anna Kalinina

Influence of the jet flowing from a gas generator through a narrow slit on shock-wave structure of a stream in the channel of variable section is investigated. Influence of the size of a jet, density and speed of gas on an entrance, and also influence of oscillations of parameters of a jet is studied. Possibility of management of a supersonic stream of shock-wave structure in the channel with the help pulse and periodic an energy supply before a jet is investigated at negative feedback on pressure.


1986 ◽  
Vol 20 (6) ◽  
pp. 846-851 ◽  
Author(s):  
A. I. Zhmakin ◽  
Yu. N. Makarov

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