Add to ORKGSYNOPSIS The unsteady flow field above a NACA 0012 airfoil oscillating in pitch has been investigated at a Reynolds number of Re = 373.000 and a reduced frequency of omega * = 0.3 by means of Particle Image Velocimetry in the subsonic wind tunnel of the ISL. Instantaneous flow fields could be measured under dynamic stall conditions, due to the short measuring time of only a few microseconds as required by the PIV technique. The results show the strong unsteady behaviour of the flow above the airfoil, especially in the downstroke motion
Unsteady aerodynamics is gaining considerable importance in this country, however, the physics of su...
This paper presents our work of an experimental examination of the flow over a NACA 0012 Airfoil at ...
ICIASF '89 RECORD, IEEE Publication 89CH2762-3, pp. 29-37.A facility for the study of dynamic stall ...
For the first time the unsteady flow field above a airfoil airfoil oscillating in pitch has been inv...
The unsteady flow field above a NACA 0012 airfoil pitching under deep dynamic stall conditions has b...
The unsteady flowfield above a NACA 0012 airfoil pitching under deep dynamic stall conditions has be...
The unsteady flow field in the wake of an NACA 23012 pitching airfoil was investigated by means of t...
The unsteady flowfield above a NACA 0012 airfoil pitching under deep dynamic stall conditions has be...
Particle Image Velocimetry (PIV) is increasingly used to investigate unsteady velocity field instant...
Unsteady aerodynamics deals with air flows that can not be sufficiently described without considerin...
The unsteady flow past a NACA 0012 airfoil that is undertaking a constant-rate pitching up motion is...
The present paper aims to investigate numerically small amplitude oscillation of NACA 0012 airfoil a...
The results of a comprehensive experimental campaign are compared to computational fluid dynamics si...
Wind tunnel experiments were carried out at low speed aerodynamics lab at IIT Kanpur to investigate ...
Unsteady aerodynamics is gaining considerable importance in this country, however, the physics of su...
Unsteady aerodynamics is gaining considerable importance in this country, however, the physics of su...
This paper presents our work of an experimental examination of the flow over a NACA 0012 Airfoil at ...
ICIASF '89 RECORD, IEEE Publication 89CH2762-3, pp. 29-37.A facility for the study of dynamic stall ...
For the first time the unsteady flow field above a airfoil airfoil oscillating in pitch has been inv...
The unsteady flow field above a NACA 0012 airfoil pitching under deep dynamic stall conditions has b...
The unsteady flowfield above a NACA 0012 airfoil pitching under deep dynamic stall conditions has be...
The unsteady flow field in the wake of an NACA 23012 pitching airfoil was investigated by means of t...
The unsteady flowfield above a NACA 0012 airfoil pitching under deep dynamic stall conditions has be...
Particle Image Velocimetry (PIV) is increasingly used to investigate unsteady velocity field instant...
Unsteady aerodynamics deals with air flows that can not be sufficiently described without considerin...
The unsteady flow past a NACA 0012 airfoil that is undertaking a constant-rate pitching up motion is...
The present paper aims to investigate numerically small amplitude oscillation of NACA 0012 airfoil a...
The results of a comprehensive experimental campaign are compared to computational fluid dynamics si...
Wind tunnel experiments were carried out at low speed aerodynamics lab at IIT Kanpur to investigate ...
Unsteady aerodynamics is gaining considerable importance in this country, however, the physics of su...
Unsteady aerodynamics is gaining considerable importance in this country, however, the physics of su...
This paper presents our work of an experimental examination of the flow over a NACA 0012 Airfoil at ...
ICIASF '89 RECORD, IEEE Publication 89CH2762-3, pp. 29-37.A facility for the study of dynamic stall ...