Aircraft Wing Tip Vortex Testing Methodology, Simulation and Analysis Techniques
24th AIAA Aerodynamic Decelerator Systems Technology Conference
01.01.2017
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Aircraft wing-tip vortex modification.
AIAA | 1973
|Flight testing of fixed-wing aircraft
TIBKAT | 2003
|