Experimental Characterization of the Hydrodynamic Interactions between a Freely Rising Bubble and a Settling Particle. [PDF]
Outokesh M +2 more
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Unsteady Aerodynamics in Bio-Inspired Flapping Wings for Low-Density Environments. [PDF]
Prisăcariu EG +8 more
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Navigating the dementia caregiving journey: A scoping review protocol of interventions and their responsiveness to caregivers' evolving needs across the illness trajectory. [PDF]
Kokorelias KM +10 more
europepmc +1 more source
Trajectory planning for drone landing, incorporating wind-sensing capabilities, operational and safety objectives, and reinforcement learning. [PDF]
Xiong H +7 more
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Experimental control of compressible OA209 dynamic stall by air jets
Gardner, A.D. +3 more
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Evaluating Dynamic Stall-Onset Criteria for Mixed and Trailing-Edge Stall
AIAA Journal, 2022We evaluate two leading-edge-based dynamic stall-onset criteria (namely, the maximum magnitudes of the leading-edge suction parameter and the boundary enstrophy flux) for mixed and trailing-edge stall. These criteria have been shown to successfully predict the onset of leading-edge stall at Reynolds numbers of [Formula: see text], where the leading ...
Sarasija Sudharsan +2 more
openaire +2 more sources
Compressibility effects on dynamic stall [PDF]
Abstract Dynamic stall delay of flow over airfoils rapidly pitching past the static stall angle has been studied by many scientists. However, the effect of compressibility on this dynamic stall behavior has been less comprehensively studied. This review presents a detailed assessment of research performed on this subject, including a historical ...
Carr, L.W., Chandrasekhara, M.S.
openaire +3 more sources
Investigation of dynamic stall onset
Aerospace Science and Technology, 2006Abstract In a 2003 test campaign in the DLR-VAG test stand unsteady pressure distributions during dynamic stall have been measured on a 2D-wing model with OA312 airfoil section. To investigate the effect of transition on dynamic stall onset different tripping devices have been fixed at the leading edge of the model.
W Geissler
exaly +3 more sources
The present work examines the influence of blade thickness-to-chord ratio (t/c) on dynamic stall phenomenon in an H-type Darrieus wind rotor. A 2D incompressible numerical study is conducted on a single-bladed rotor at a tip speed ratio (TSR) of 2 with a
Siddhant Jain, Ujjwal K Saha
exaly +2 more sources

