The Effect of Pulsed Sliding Surface Discharges on Supersonic Airflow past a Thin Wedge in Shock Tube

2018 ◽  
Vol 44 (2) ◽  
pp. 157-159 ◽  
Author(s):  
I. V. Mursenkova ◽  
A. S. Sazonov ◽  
Yu. Liao
Keyword(s):  
Shock Tube ◽  
Sliding Surface ◽  
Supersonic Airflow ◽  
Surface Discharges ◽  
Thin Wedge

scholarly journals Влияние импульсных скользящих поверхностных разрядов на сверхзвуковое обтекание тонкого клина в ударной трубе

2018 ◽  
Vol 44 (4) ◽  
pp. 59
Author(s):  
И.В. Мурсенкова ◽  
А.С. Сазонов ◽  
Ю. Ляо
Keyword(s):  
Shock Waves ◽  
Stationary Flow ◽  
Density Field ◽  
Surface Discharge ◽  
Sliding Surface ◽  
Flow Past ◽  
Wedge Surface ◽  
Rear Part ◽  
Surface Discharges ◽  
Thin Wedge

AbstractThe influence of ~300-ns pulsed sliding surface discharges on supersonic airflow with M = 1.2–1.5 past a thin wedge has been studied in a shock tube at 0.12–0.14 kg/m^3 gas density. It is established that inhomogeneity of the airflow-density field near the wedge leads to changes in the discharge current geometry and the structure of surface-discharge glow. The dynamics of discharge-initiated shock waves disturbing the quasi-stationary flow past the wedge was studied by the method of shadow visualization. It is shown that shock waves from intense surface-discharge channels in front of the wedge and behind its rear part can produce nonstationary action on the flow past the wedge surface, which lasts for up to 120 μs after the discharge pulse.

The development of weak waves in the steady two-dimensional flow of a gas with vibrational relaxation past a thin wedge

1975 ◽  
Vol 69 (1) ◽  
pp. 109-128 ◽  
Author(s):  
R. P. Hornby ◽  
N. H. Johannesen
Keyword(s):  
Supersonic Flow ◽  
Shock Tube ◽  
Small Angle ◽  
Vibrational Relaxation ◽  
Method Of Characteristics ◽  
Numerical Solutions ◽  
Two Dimensional ◽  
Wave Decay ◽  
Two Dimensional Flow ◽  
Thin Wedge

The method of characteristics is used to calculate the supersonic flow past a wedge of small angle with non-equilibrium effects. The wave decay and development distances are presented in a concise similarity form which permits accurate extrapolation to very weak waves. The numerical solutions are compared with shock-tube flows of CO2 and N2O.

The Characteristics of a Nanosecond Surface Sliding Discharge in a Supersonic Airflow Flowing around a Thin Wedge

2019 ◽  
Vol 74 (3) ◽  
pp. 269-276 ◽  
Author(s):  
I. V. Mursenkova ◽  
Yu. Liao ◽  
I. E. Ivanov ◽  
N. N. Sysoev
Keyword(s):  
Supersonic Airflow ◽  
Sliding Discharge ◽  
Thin Wedge

Using a shock tube to predict the response of polymeric foam to a blast loading

2006 ◽  
Vol 134 ◽  
pp. 783-787 ◽  
Author(s):  
S. Ouellet ◽  
D. Frost ◽  
A. Bouamoul
Keyword(s):  
Shock Tube ◽  
Blast Loading ◽  
Polymeric Foam

Pyrolysis of methane in a single pulse shock tube

1972 ◽  
Vol 22 (3) ◽  
pp. 303-317 ◽  
Author(s):  
D. H. Napier ◽  
N. Subrahmanyam
Keyword(s):  
Shock Tube ◽  
Single Pulse

WATER SHOCK TUBE SIMULATION WITH TAIT EQUATION OF STATE

2018 ◽  
Author(s):  
Jishnu Chandran R. ◽  
Abdusamad Salih
Keyword(s):  
Equation Of State ◽  
Shock Tube ◽  
Tait Equation ◽  
Tait Equation Of State
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