Transactions of Nanjing University of Aeronautics & Astronautics
Archive > Volume 36 Issue 5 > 2019,36(5):747-759. DOI:10.16356/j.1005-1120.2019.05.006 Prev Next

Analysis and Calibration of Internal Flow Force of Ejector-Powered Engine Simulator System in Wind Tunnels

CHINA AERO-SCIENCES

WeChat

Mobile website

Close