A complex of wind tunnels and gas dynamic facilities operating in the Institute covers the Mach number range from 0.01 to 25 and the Reynolds number range from 10^4 to 10^8. A unique hypersonic wind tunnel of adiabatic compression with pressure multipliers is under construction. This wind tunnel will ensure the full-scale Reynolds numbers and a pure flow with constant parameters and rather long running time. The main parameters of the facilities are presented in the table and plotted in the graph.

Wind tunnels