This paper has developed a mathematical model for calculating the conjugate heat transfer
between a supersonic airflow at the freestream Mach numbers M∞= 3, 4, 5, and a copper …

Results of simulations of supersonic turbulent flows in a channel with allowance for
conjugate heat transfer between the air flow and a copper plate modeling the sensitive …

Methodological aspects of stagnation-temperature measurement in high-enthalpy
supersonic air flows using a thermoelectric transducer (thermocouple) with shielded …

The paper presents the results of numerical simulations of high-velocity turbulent air flows in
a plane channel with a variable cross section exhibiting sudden expansion with allowance …

Heat exchange of a blunt cylinder in a hypersonic (M= 6) air flow are studied numerically.
Calculations are carried out in ANSYS Fluent, taking into account the conjugate heat transfer …

Existence and intensive growth of heat flux on a vehicle is one of the main problems in
hypersonic flight. Experimental study of heat flux in the stagnation point of a blunt cylinder in …

Experimental results are given for separated supersonic flow influence on adiabatic wall
temperature of the plane surface. Separated flow was generated by a falling shock wave in …

This paper describes a problem of measuring a gas flow temperature using thermocouples
for which the time it takes to reach an equilibrium temperature is shorter than the duration of …

We present the results of comparative measurements of the heat flux to a flat plate in a
supersonic flow at a Mach number of M= 6, which were performed using the two following …

The results of an experimental study of heat transfer for supersonic flow around plane
surface in the wake of a rib are presented. The study was conducted on unsteady regime …