Results 21 to 30 of about 4,618,854 (237)
The dynamic stall phenomenon is characterized by the formation of a leading-edge vortex, which is responsible for adverse aerodynamic forces and moments adversely impacting the structural strength and life of a system. Aerodynamic shape optimization (ASO)
Vishal Raul, Leifur Þ. Leifsson
semanticscholar +1 more source
Analysis of the onset and evolution of a dynamic stall vortex on a periodic plunging aerofoil
The onset and evolution of the dynamic stall vortex (DSV) are analysed by means of large eddy simulations of an SD7003 aerofoil undergoing periodic plunging motion in a transitional Reynolds number flow ($Re =6\times 10^{4}$).
R. Miotto +3 more
semanticscholar +1 more source
Experimental Study of Dynamical Airfoil and Aerodynamic Prediction
Dynamic stall is a critical limiting factor for airfoil aerodynamics and a challenging problem for active flow control. In this experimental study, dynamic stall was measured by high-frequency surface pressure tapes and pressure-sensitive paint (PSP ...
Zheyu Shi +3 more
doaj +1 more source
Numerical Simulation of a Pitching Airfoil Under Dynamic Stall of Low Reynolds Number Flow [PDF]
In this research, viscous, unsteady and turbulent fluid flow is simulated numerically around pitching NACA0012 airfoil in the dynamic stall area. The Navier-Stokes equations are discretized based on the finite volume method and are solved by the PIMPLE ...
Mojtaba Honarmand +3 more
doaj +2 more sources
Recent seismic imaging of the mantle beneath western North America reveals complexities interpreted as structures ranging from plumes to lithospheric drips and slab fragments. A prominent high-velocity "curtain" beneath Idaho has been interpreted as a remnant of the subducted Farallon plate left dangling within the upper mantle since >40 Ma ...
Burkett, Erin, Gurnis, Michael
openaire +2 more sources
Study on the effect of raindrops on the dynamic stall of a NACA-0012 airfoil
In this study the pure effect of raindrops on dynamic stall of a pitching airfoil has been investigated. The simulation was performed at Reynolds number of 106\documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts ...
Armin Sheidani +2 more
semanticscholar +1 more source
A vorticity-based criterion to characterise leading edge dynamic stall onset
We propose a more conservative, physically-intuitive criterion, namely, the boundary enstrophy flux ($BEF$), to characterise leading-edge-type dynamic stall onset in incompressible flows.
S. Sudharsan +2 more
semanticscholar +1 more source
Dynamic Stall Measurements [PDF]
AbstractForces acting statically on an airfoil in laminar flow are well known. Under turbulent conditions dynamic effects (like dynamic stall) take place. There are different theoretical models to describe dynamic stall, but very little experimental data.
Jörge Schneemann +2 more
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The current design of vertical axis wind turbines (VAWTs) suffers from inevitable change in tip speed ratio, λ, in variant wind conditions due to fixed rotor speed.
M. R. Tirandaz, A. Rezaeiha
semanticscholar +1 more source
The effects of turbulence modeling on dynamic stall [PDF]
A numerical investigation of the flow evolution over a pitching NACA 0012 airfoil incurring in deep dynamic stall phenomena is presented. The experimental data at Reynolds number Re = 135, 000 and reduced frequency k = 0.1, provided by Lee and Gerontakos,
G. Baldan +3 more
semanticscholar +1 more source

