A study was done of the phenomena concerning profiles in dynamic stall configuration, and more specially those related to pitch oscillations. The most characteristic experimental results on flow separations with a vortex character, and their repercussions on local pressures and total forces were analyzed. Some aspects of the methods for predicting flows with the presence (or not) of boundary layer separation are examined, as well as the main simplified methods available to date for the calculation of total forces in such configurations
An effort to understand and control the unsteady separated flow associated with the dynamic stall of...
The effect of the unsteady motion of an airfoil on its stall behavior is of considerable interest to...
A series of wind tunnel experiments were conducted on an NACA 0012 airfoil undergoing a linear pitch...
The general features of dynamic stall on oscillating airfoils are explained in terms of the vortex s...
A method for analyzing unsteady airfoil stall was refined by including nonlinear effects in the repr...
Experimental and computational investigations of the dynamic stall phenomenon continue to attract th...
International audienceDynamic stall is a highly complex phenomenon characterized by unsteady massive...
Among the new significant aspects of the present work are: (1) the treatment of the far-field bounda...
The dynamic stall flow field over NACA 0012 airfoil pitching transiently from 0 - 60 at a constant r...
A modification of the viscous-inviscid interaction concept with the employment of coupled vortices a...
The flow over a NACA 0012 airfoil undergoing large oscillations in pitch was experimentally studied ...
Experimental and computational investigations of the dynamic stall phenomenon continue to attract th...
The dynamic stall phenomenon was examined in detail by analyzing an existing set of unsteady pressur...
The article of record as published may be found at http://dx.doi.org/10.2514/6.1993-211The dynamic s...
The research was carried out in the Compressible Dynamic Stall Facility, CDSF, at the Fluid Mechanic...
An effort to understand and control the unsteady separated flow associated with the dynamic stall of...
The effect of the unsteady motion of an airfoil on its stall behavior is of considerable interest to...
A series of wind tunnel experiments were conducted on an NACA 0012 airfoil undergoing a linear pitch...
The general features of dynamic stall on oscillating airfoils are explained in terms of the vortex s...
A method for analyzing unsteady airfoil stall was refined by including nonlinear effects in the repr...
Experimental and computational investigations of the dynamic stall phenomenon continue to attract th...
International audienceDynamic stall is a highly complex phenomenon characterized by unsteady massive...
Among the new significant aspects of the present work are: (1) the treatment of the far-field bounda...
The dynamic stall flow field over NACA 0012 airfoil pitching transiently from 0 - 60 at a constant r...
A modification of the viscous-inviscid interaction concept with the employment of coupled vortices a...
The flow over a NACA 0012 airfoil undergoing large oscillations in pitch was experimentally studied ...
Experimental and computational investigations of the dynamic stall phenomenon continue to attract th...
The dynamic stall phenomenon was examined in detail by analyzing an existing set of unsteady pressur...
The article of record as published may be found at http://dx.doi.org/10.2514/6.1993-211The dynamic s...
The research was carried out in the Compressible Dynamic Stall Facility, CDSF, at the Fluid Mechanic...
An effort to understand and control the unsteady separated flow associated with the dynamic stall of...
The effect of the unsteady motion of an airfoil on its stall behavior is of considerable interest to...
A series of wind tunnel experiments were conducted on an NACA 0012 airfoil undergoing a linear pitch...