We present a fully discrete approximation technique for the compressible Navier–Stokes
equations that is second-order accurate in time and space, semi-implicit, and guaranteed to …

The study is devoted to assessing the applicability of the manufactured thermoelectric
sensor for functioning in shock tubes to measure instantaneous heat fluxes occurring in …

The flow in a shock tube is extremely complex with dynamic multi-scale structures of sharp
fronts, flow separation, and vortices due to the interaction of the shock wave, the contact …

Development of two-dimensional model, has been focused on the SCHOLAR experiment.
Convective and radiative heating the inner surface of the chamber scramjet have been …

Abstract Models of the ExoMars spacecraft [1-3] and variants of the X-43 air intake [4-9] were
first tested in the hypersonic aerodynamic shock tube (HAST)[10-13] facility. The shock-wave …

The temperature gradient fields of a wedge with double ramp were explored by using
applied method temperature sensitive paint [1-4]. The model was studied experimentally in …

I. Introduction hysical gas dynamic investigations are of great importance for studies of
physical and mechanical processes that occur near the bodies of aerospace vehicles and …

Shock-wave experiments with aerodynamic primitives in the form of a half wedge/double
wedge with blunt edges are performed. Experimental studies were conducted using models …

I. Introduction low pressure manometer based on the high-voltage, low-pressure plasma
discharge placed in axial magnetic field was proposed in 1937 by FM Penning. 1 Later it …

The numerical simulation of influence of viscous effects on flow inside shock tubes are
described. We considered three shock tubes with different length-to-height ratio: 1 to 1 (Daru …