AN INTERNATIONAL RESEARCH PERSPECTIVE ON AIRSPACE INTEGRATION IN THE FRAMEWORK OF URBAN AIR MOBILITY
Mach Number Effect on Aeroacoustic Characteristics of Compressible Jet Due to Chevron
AIRCRAFT SYSTEMS ARCHITECTING: LOGICAL-COMPUTATIONAL DOMAIN INTERFACE
Control of Low Speed Cavity Flow Using Streamwise Tabs at Leading Edge (AIAA 2017-0948)
An unmanned marine vehicle thruster fault diagnosis scheme based on OFNDA