The invention discloses a low-speed compact wind tunnel experimental device suitable for building outdoor wind environment testing, which comprises a matrix fan
system and a modularized segmented structure (sequentially comprising an air inlet section, a rectification section, a model placement area and an air outlet section), and all the sections are connected through
flange plates and sealing parts to guarantee the sealing performance. Wherein the matrix fan
system is composed of 4 * 4 fans, each fan is subjected to independent
frequency modulation through a frequency converter, and the
airflow speed is actively adjusted; each section in the modularized segmented structure is an independent module; the air inlet section is used for mixing
jet flow generated by the
matrix type fan
system; a plurality of rectifying parts are arranged in the rectifying section, and the uniformity, turbulence intensity and
wind speed gradient of
airflow are passively adjusted by configuring different parts, so that specific
wind field environment characteristics required by an experiment are accurately simulated; the model placing area is provided with a rotatable disc used for placing a building reduced
scale model required by an experiment. The air outlet section is located at the
tail end of the wind tunnel experiment device and is provided with an
airflow outlet with an adjustable cross section area.