The developed and tested visualisation method of supersonic under-expanded gas jets
expanding from sonic and supersonic nozzles (or nozzle blocks) into a rarefied medium …

The functionality of" Hypersonic aerodynamic shock tube" facility was expanded to obtain
more complete validation of developed computer codes for the prospective high-speed …

This article presents the results of the heat flux measurement on a flat channel plate and a
cylinder within a gas stream. The developed calorimetric sensors are used simultaneously …

Аэротермодинамика фрагментов высокоскоростных аппаратов экспериментально
исследовалась на моделях в лабораторной установке кратковременного действия …

Приведены результаты экспериментальных исследований по регистрации
радиационной составляющей полного теплового потока термоэлектрическим …

The variety of studies on shoc+-wave interactions in a channel simulating the air inta+ e of
high-speed aircraft (HSA) shows an increasing number of computational and experimental …

A series of experiments were performed by using following geometric primitives and its
combinations: sharp and blunt edges, wedge, half-length with" flamholder" or" bump" …

Specialists from TsAGI have developed a unique two-channel luminescent transducer, a
temperature-sensitive paint that allows the measurement of full-field surface heat transfer …

The functionality of the more complete validation of the developed CDF is being expanded
for" Hypersonic aerodynamic shock tube" laboratory facilities. Models of triple semi-wedge …

(Computational Fluid Dynamics—Вычислительная гидрогазодинамика) пакета «ANSYS
Fluent». В процессе работы рассматриваются характеристики процессов КС до и после …