The Rise of Forces on a Wedge during the Interaction of a Sliding Discharge with a Supersonic Flow

2021 ◽  
Author(s):  
V. M. Bocharnikov ◽  
V. V. Golub ◽  
A. S. Savel’ev
Keyword(s):  
Supersonic Flow ◽  
Sliding Discharge

scholarly journals Возникновение усилий на клине при взаимодействии скользящего разряда со сверхзвуковым потоком

2021 ◽  
Vol 47 (9) ◽  
pp. 33
Author(s):  
В.М. Бочарников ◽  
В.В. Голуб ◽  
А.С. Савельев
Keyword(s):  
Shock Wave ◽  
Reynolds Number ◽  
Mach Number ◽  
Supersonic Flow ◽  
Wind Tunnel ◽  
Static Pressure ◽  
Discharge Energy ◽  
Pulse Heat ◽  
The Impact ◽  
Sliding Discharge

It was investigated generation of forces on the wedge during the interaction of a sliding discharge in the supersonic flow. Sliding discharge was generated in a supersonic atmospheric-vacuum wind tunnel with a flow Mach number M = 2, Reynolds number of about 106, and static pressure in the flow p = 0.15 bar. It was found that the impact of the discharge is not limited by the appearance of a shock wave, and also significantly changes the properties of the flow around the wedge due to pulse heat generation. As the discharge energy increases, the force from its impact on the wedge also increases. Force produced by the sliding discharge in the supersonic flow is several times greater than in the quiescent air regardless of its pressure: 0.15 bar or 1 bar.

Numerical Studies on Behavior of Lorentz-Force-Applied Boundary Layer in Supersonic Flow

2009 ◽  
Vol 129 (6) ◽  
pp. 831-839
Author(s):  
Keisuke Udagawa ◽  
Sadatake Tomioka ◽  
Hiroyuki Yamasaki
Keyword(s):  
Boundary Layer ◽  
Supersonic Flow ◽  
Lorentz Force ◽  
Numerical Studies

IMPROVEMENT OF FLAMEHOLDING CHARACTERISTICS BY INCIDENT SHOCK WAVES IN SUPERSONIC FLOW

2002 ◽  
Vol 5 (1-6) ◽  
pp. 330-339 ◽  
Author(s):  
T. Fujimori ◽  
M. Murayama ◽  
J. Sato ◽  
H. Kobayashi ◽  
S. Hasegawa ◽  
...  
Keyword(s):  
Supersonic Flow ◽  
Shock Waves ◽  
Incident Shock
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