Researches of dorsal support interference in low speed wind tunnel thrust vector test;

Experimental research on quick speed-changing device for low speed wind tunnel;

Investigation of civil airplane force measurement in low speed wind tunnel;

Study on low speed wind power system;

Study on the test uncertainty level at high angles of attack for domestic capital low-speed wind tunnels;

In this paper,a small-size model bracket used in the low-speed wind tunnel experiment of MAV(micro air vehicle) is designed.

Based on the aerodynamic test of plane models under different positions,the variable angle system used in low-speed wind tunnels is designed in this paper.