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Vorticity Transport Analysis on Blunt Trailing-Edge Blades in Reverse Flow

Journal of Aircraft
High-advance-ratio rotorcraft face reverse flow effects on a substantial portion of the retreating blades. Similar to a leading-edge vortex, the reverse flow dynamic stall vortex was found to have a significant impact on unsteady blade loading and pitching moment evolution due to its strength and proximity to the blade surface.
Oliver D. Wild   +2 more
openaire   +1 more source

Thermal-hydraulic performance of additively manufactured lattices for gas turbine blade trailing edge cooling

Applied Thermal Engineering, 2022
Inderjot Kaur   +2 more
exaly  

Trailing Edge Noise of Innovative Mini-RPA Propeller Blade Geometry

2018 AIAA/CEAS Aeroacoustics Conference, 2018
Halimi Akila   +2 more
openaire   +1 more source

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