EXPERIMENTAL STUDY ON DISCHARGE COEFFICIENT OF WING BOX CHANNEL IN CIVIL AIRCRAFT
CSAA/IET International Conference on Aircraft Utility Systems ; 2020 ; Online
2021
Conference paper
English
Penetrating High Wing Structure of Civil Aircraft with Blended-Wing-Body
European Patent Office | 2022
|Wing design for a civil tiltrotor transport aircraft
NTRS | 1994
|Characterisation of Buffet on a Civil Aircraft Wing
AIAA | 2016
|