The invention provides a
pressure measurement tail rake for a
wing section tunnel test. Two ends of a cross beam are fixed at the top of a support; a plurality of
pressure measurement cones are respectively arranged above the cross beam through a rotating shaft; the
pressure measurement cones are streamlined bodies of revolution, and after the aerodynamic center of the pressure measurement cones is arranged at the pressure measurement cone
support point, the direction of incoming flow can be captured, and the
direction angle of the incoming flow can be measured by angular transducers arranged at the bottom of the cross beam and the lower end of the rotating shaft; a total pressure hole is arranged at the head part of each pressure measurement cone, and a static pressure hole is arranged on the upper surface, a certain distance behind the head part of each pressure measurement cone, one end of a pressure measurement
pipe is guided into the total pressure hole and the static pressure hole through the rotating shaft, the other end of the pressure measurement
pipe is connected with a
pressure data acquisition
system, and therefore, the pressure measurement
pipe can be used for measuring the total pressure of
airflow and the pressure of the static pressure hole, the two-dimensional velocity distribution in the cross
beam direction can be calculated, and the resistance of a
wing section model in front of the
tail rake can be calculated further. The pressure measurement
tail rake can be used for accurately measuring the total pressure of
airflow at the pressure measurement cones, as well as the velocity, drift angles and two velocity components of
airflow at the pressure measurement cones, thereby obtaining the resistance and lift force which act on the
wing section model.