Vortex Identification and Quantification on Blunt Trailing-Edge Rotor Blades in Reverse Flow
An inherent aerodynamic limitation of high-advance-ratio high-speed helicopters is reverse
flow on the retreating blades, which can be a source of several unsteady effects, like vortex …
flow on the retreating blades, which can be a source of several unsteady effects, like vortex …
Vortex Identification and Quantification on Blunt Trailing-Edge Rotor Blades in Reverse Flow
OD Wild, AR Jones - AIAA Journal, 2023 - ui.adsabs.harvard.edu
An inherent aerodynamic limitation of high-advance-ratio high-speed helicopters is reverse
flow on the retreating blades, which can be a source of several unsteady effects, like vortex …
flow on the retreating blades, which can be a source of several unsteady effects, like vortex …