Tests were made based on C919 commercial aircraft model.

Experiment setup in the 1.2m subsonic wind tunnel of China Academy of Aerospace Aerodynamics

Flow characteristics on the nose of the aircraft
HUANG Zhan, Zhangjiang, Zhang Weimin, Li Lang, Dongjin Gang, Mao Tao, Wang Hongwei
China Academy of Aerospace Aerodynamics, Beijing

The objective was to test different aircraft nose flow characteristics to compare the pros and cons of different designs and suggest the best nose design. In China Institute of Aerospace Aerodynamics 1.2 m super middleweight Asia across a certain type of aircraft wind tunnel.