In the paper a historical overview of scramjet propulsion development is presented. Three
main stages of development of hypersonic summer programs are distinguish. The …

In the paper three-dimensional model for hypersonic flow are described. Comparing the
result of calculation with wall pressure data, obtained in the inlet-isolator model mounted to …

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 …

In the paper two-dimensional model for hypersonic flow are described. Comparing the result
of calculation with wall pressure data, obtained in the inlet-isolator model mounted to the …

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 …

In this paper we present a concept and implementation details of a new visualization
subsystem for presentation of the results of scientific computations. The subsystem is built …

This paper presents the general idea and the first implementation of the new visualization
system–an integrated environment for viewing and analyzing results of aerogasdynamic …

The work studies the influence of a growing boundary layer on the process of the supersonic
flow around an aerodynamic body. The task is to select and implement in an experiment the …

The features of 3D printing method for rapid prototyping and manufacturing of models for a
pulsed high-speed gas-dynamic experiment are considered. Modern additive technologies …