The present invention belongs to the technical field of flow field testing, and discloses a full-parameter probe for measuring the two-dimensional steady flow field of the boundary layer on the outer wall of a hub, which includes a probe head,
pressure sensing holes, a temperature sensor, an adiabatic and insulating seal, a pressure guiding tube, a temperature sensor cable, a temperature sensor cable lead-out channel, a pressure guiding tube lead-out channel, and a probe strut. The probe head is cylindrical, and three non-connecting
pressure sensing holes arranged in a "pin" shape are disposed on the windward surface; an arc groove is axially formed on the leeward surface of the probe head, and the temperature sensor is placed in the arc groove to avoid the direct
impact of the mainstream on the temperature sensor. Compared with the existing boundary layer probes, the present invention can simultaneously measure the total temperature, static temperature, total pressure, static pressure,
deflection angle, Mach number, density, and two-dimensional velocity of the two-dimensional steady flow field in the boundary layer on the outer wall of the hub, and can also take into account the measurement of the flow field in the boundary layer in the inlet of an aeroengine, and has the characteristics of small size,
high spatial resolution, high measurement accuracy, and high reliability.