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 …

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 …

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 …

В работе представлен опыт создания программного комплекса hySol,
предназначенного для моделирования высокоскоростных течений при наличии …

A three-dimensional numerical simulation of 25/55 double-cone high-speed
aerothermodynamics on an unstructured grid was carried out. For numerical simulation of …

The paper presents the experience of developing the hySol software package intended for
numerical simulation of high–speed flows in the presence of a complex shock–wave …

The effectiveness of porous bleeders in mitigating unstart phenomena and improving
isolator performance in a hypersonic scramjet was investigated. Through CFD simulations …

A high-fidelity CFD code hySol is developed based on high resolution Godunov method to
simulate supersonic flows using 3D unstructured grids. It is designed for accurately …

The results of investigations of the conical nozzle block of the hypersonic shock
aerodynamic tube (HAST)[1–4] of the Laboratory of Radiative Gas Dynamics of the Institute …