Effect of structure of a surface supersonic flow on the stabilization of a flame behind the base of an axisymmetric body

1975 ◽  
Vol 9 (5) ◽  
pp. 631-634
Author(s):  
V. K. Baev ◽  
A. V. Lokotko ◽  
P. K. Tret'yakov
Keyword(s):  
Supersonic Flow ◽  
Axisymmetric Body ◽  
Effect Of Structure

The Effect of Sting Diameter and Length on Base Pressure at M = 3·88

1968 ◽  
Vol 19 (4) ◽  
pp. 368-374 ◽  
Author(s):  
Walter R. Sieling
Keyword(s):  
Supersonic Flow ◽  
Axisymmetric Body ◽  
Base Pressure ◽  
Base Diameter ◽  
Apparent Change

SummaryThe effects of sting diameter and cylindrical protuberance length on the base pressure of an axisymmetric body in a turbulent supersonic flow are experimentally determined. It is found that the change in base pressure due to the presence of the sting is greater than 4 per cent when the ratio of sting diameter to base diameter is 0·150 or greater. When the ratio of cylindrical protuberance length to base diameter is greater than 1·3 there is no apparent change in base pressure with a change in length. However, when this ratio is less than 1·3, the base pressure varies greatly with length.

Supersonic flow around a hemi-axisymmetric body resting on a flat plate.

AIAA Journal ◽  
1965 ◽  
Vol 3 (11) ◽  
pp. 2152-2154
Author(s):  
STEVEN S. CHERRY
Keyword(s):  
Supersonic Flow ◽  
Flat Plate ◽  
Axisymmetric Body

Experimental investigation of three-dimensional supersonic flow past an axisymmetric body with an annular cavity

2014 ◽  
Vol 49 (4) ◽  
pp. 540-546 ◽  
Author(s):  
S. V. Guvernyuk ◽  
A. F. Zubkov ◽  
M. M. Simonenko ◽  
A. I. Shvetz
Keyword(s):  
Experimental Investigation ◽  
Supersonic Flow ◽  
Three Dimensional ◽  
Axisymmetric Body ◽  
Flow Past
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