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How DNA secondary structures drive replication fork instability.
Sethi A +3 more
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Optimal fuzzy-PID controller design for object tracking. [PDF]
Melese YL, Alitasb GK, Belete MD.
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Research on a Visually Assisted Efficient Blind-Guiding System and an Autonomous Shopping Guidance Robot Arm Adapted to the Complex Environment of Farmers' Markets. [PDF]
Liu M +5 more
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Comparison of Nose Wipes, Stall Sponges, and Air Samples with Nasal Secretions for the Molecular Detection of Equine Influenza Virus in Clinically and Subclinically Infected Horses. [PDF]
Pusterla N +3 more
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UnitedXR Europe 2025: Aligning Health Care Extended Reality.
Costa JF.
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Dynamic stall simulation problems
Guidance, Control and Flight Mechanics Conference, 1970Dynamic airfoil stall simulation in wind tunnels, considering pitch rate, Reynolds number, oscillation and test equipment ...
LARS E. ERICSSON, J. PETER REDING
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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
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Dynamic Stall and Aerodynamic Damping
Journal of Solar Energy Engineering, 1998Riso̸ has developed a dynamic stall model that is used to analyze and reproduce open air blade section measurements as well as wind tunnel measurements. The dynamic stall model takes variations in both angle of attack and flow velocity into account. The paper gives a brief description of the dynamic stall model and presents results from analyses of ...
Flemming Rasmussen +2 more
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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.
Geissler, Wolfgang, Haselmeyer, Hartmut
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