Numerical calculation of supersonic flow about ducted bodies at an angle of attack

1967 ◽  
Vol 2 (3) ◽  
pp. 81-84
Author(s):  
O. N. Katskova ◽  
P. I. Chushkin
Keyword(s):  
Numerical Calculation ◽  
Supersonic Flow ◽  
Angle Of Attack

Supersonic flow past a sharp cone oscillating about a zero angle of attack

1998 ◽  
Vol 33 (6) ◽  
pp. 913-923
Author(s):  
Yu. M. Lipnitskii ◽  
E. V. Matsyura ◽  
A. N. Pokrovskii
Keyword(s):  
Supersonic Flow ◽  
Angle Of Attack ◽  
Flow Past ◽  
Sharp Cone

Effect of angle of attack on supersonic flow past axisymmetric blunt bodies with surface injection

1988 ◽  
Vol 22 (5) ◽  
pp. 737-742 ◽  
Author(s):  
V. A. Antonov ◽  
A. M. Grishin ◽  
F. M. Pakhomov
Keyword(s):  
Supersonic Flow ◽  
Angle Of Attack ◽  
Flow Past ◽  
Blunt Bodies

scholarly journals Comparative analysis of OpenFOAM solvers for the problem of supersonic flow around a cone at an angle of attack

2020 ◽  
pp. 1-12
Author(s):  
Alexander Evgenyevich Bondarev ◽  
Artyom Evgenyevich Kuvshinnikov ◽  
Tatiana Nikolaevna Mikhailova ◽  
Irina Gennadievna Ryzhova
Keyword(s):  
Comparative Analysis ◽  
Supersonic Flow ◽  
Angle Of Attack ◽  
Flow Around A Cone

Numerical Simulation of Lateral Jet Interaction a Slender Body in Supersonic Flow

2013 ◽  
Vol 404 ◽  
pp. 296-301
Author(s):  
Shi Jie Luo ◽  
Yao Feng Liu ◽  
Ning Cao
Keyword(s):  
Supersonic Flow ◽  
Angle Of Attack ◽  
Symmetry Plane ◽  
Slender Body ◽  
Lateral Loads ◽  
Jet Interaction ◽  
Pressure Distributions ◽  
Highly Nonlinear ◽  
Flow Features ◽  
Force Moment

A numerical investigation has been conducted to research the interaction flowfield of lateral jet not in the longitudinal symmetry plane on a slender body with rudders in supersonic flow. The surface and space flow features of jet interaction flowfield with different angles of attack was analyzed. The paper also compared with and without jet interaction flowfield characteristics. As a result, the jet interaction destroys pressure distributions of the slender body, and causes normal and lateral loads. With angle of attack, the pressure distributions of the after body and rudders surfaces are change tempestuously. The results also show that the far-field interference played a major role in the lateral jet interaction. Besides, the force/moment amplification factors present highly nonlinear with angle of attack.

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