Hartmann–Sprenger effect and its application on aircraft

Abstract

The question of the effect of viscosity on the occurrence of a stagnation temperature in a dead-end cavity above the deceleration temperature of the incident gas flow the so-called Hartmann–Sprenger effect is considered. It is shown that the Hartmann–Sprenger effect can be used to create the design of the anti-icing system of the aircraft

Keywords

• hartmann–sprenger effect
• viscosity
• kinetic energy
• aircraft
• anti-icing system