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 …
Flow structure of low-aspect-ratio rotating wings from dye visualization
ZR Carr, MJ Ringuette - AIAA journal, 2014 - arc.aiaa.org
EFFORTS to develop bioinspired micro air vehicles (MAVs) have motivated flapping-wing
aerodynamics research (see Shyy et al.[1]). The focus of this Note is simplified wings of low …
aerodynamics research (see Shyy et al.[1]). The focus of this Note is simplified wings of low …
Aspect ratio effects on the leading-edge circulation and forces of rotating flat-plate wings
Significant research has been focused on the unsteady fluid dynamics and forces of flapping
wings and more simplified bio-inspired configurations, in part driven by its application to …
wings and more simplified bio-inspired configurations, in part driven by its application to …