AIR PRESSURE PROBE

摘要

The invention relates to the field of aviation and to devices for determining aircraft flight parameters or wind tunnel flow parameters. The present device consists of a head part with intake holes located thereon, which are connected by channels to couplers, and a support, attached to the head part from behind. The surface of the head part is provided with vortex generators. The vortex generators can be in the form of indentations or protrusions of various shapes on the surface of the air pressure probe, or in the form of ribs formed as a result of the mating of elements of the flat or curved planes that form the surfaces of the head part and the support. The technical result is an increased operational range of measurement and a wider field of practical application.