Results 21 to 30 of about 4,618,854 (237)

Surrogate-based aerodynamic shape optimization for delaying airfoil dynamic stall using Kriging regression and infill criteria

open access: yesAerospace Science and Technology, 2021
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

open access: yesJournal of Fluid Mechanics, 2022
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

open access: yesActuators, 2022
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]

open access: yesJournal of Aerospace Technology and Management, 2019
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

Stalled slab dynamics [PDF]

open access: yesLithosphere, 2013
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

open access: yesJournal of the Brazilian Society of Mechanical Sciences and Engineering, 2022
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

open access: yesJournal of Fluid Mechanics, 2022
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]

open access: yesPAMM, 2009
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
openaire   +1 more source

Effect of airfoil shape on power performance of vertical axis wind turbines in dynamic stall: Symmetric Airfoils

open access: yes, 2021
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]

open access: yesActa Mechanica
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

Home - About - Disclaimer - Privacy