An Experimental Investigation of Supersonic Flow Past Yawed Cones

1971 ◽  
Author(s):  
Rafael Yahalom
Keyword(s):  
Experimental Investigation ◽  
Supersonic Flow ◽  
Flow Past

Experimental investigation of supersonic flow past blunt bodies with strong distributed injection

1978 ◽  
Vol 13 (3) ◽  
pp. 406-415 ◽  
Author(s):  
M. A. Koval' ◽  
V. P. Stulov ◽  
A. I. Shvets
Keyword(s):  
Experimental Investigation ◽  
Supersonic Flow ◽  
Flow Past ◽  
Blunt Bodies

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

Experimental Investigation of Supersonic Flow Past Double-Wedge Configurations

AIAA Journal ◽  
1975 ◽  
Vol 13 (7) ◽  
pp. 897-901 ◽  
Author(s):  
John J. Bertin ◽  
John C. Hinkle
Keyword(s):  
Experimental Investigation ◽  
Supersonic Flow ◽  
Double Wedge ◽  
Flow Past

The Supersonic Flow Past a Slender Ducted Body of Revolution with an Annular Intake

1950 ◽  
Vol 1 (4) ◽  
pp. 305-318
Author(s):  
G. N. Ward
Keyword(s):  
Supersonic Flow ◽  
Velocity Potential ◽  
Operational Calculus ◽  
The Body ◽  
Body Of Revolution ◽  
Internal Flows ◽  
Flow Past ◽  
External Forces ◽  
Internal Pressures ◽  
Slender Body Of Revolution

SummaryThe approximate supersonic flow past a slender ducted body of revolution having an annular intake is determined by using the Heaviside operational calculus applied to the linearised equation for the velocity potential. It is assumed that the external and internal flows are independent. The pressures on the body are integrated to find the drag, lift and moment coefficients of the external forces. The lift and moment coefficients have the same values as for a slender body of revolution without an intake, but the formula for the drag has extra terms given in equations (32) and (56). Under extra assumptions, the lift force due to the internal pressures is estimated. The results are applicable to propulsive ducts working under the specified condition of no “ spill-over “ at the intake.

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