An experimental system that generates and visualizes impulsive flow in air has been employed to visualize vortex structures and processes over airfoils at high angles of attack. The photographic sequences reveals the details of flow separation, subsequent vortex formation and the onset of steady-state vortex shedding. It is hoped that the results of this study serve as a reference on vortex structure and processes over bluff bodies in impulsive motion and as a useful guide for future measurements and parametric computer studies
AbstractVisualization test is performed at the water channel of BUAA. The vortex core is visualized ...
The formation and development of leading-edge vortices, vortex breakdown, and three-dimensional sepa...
We present the visual analysis of a biologically inspired CFD simulation of the deformable flapping ...
An experimental system that generates and visualizes unsteady motions in air was employed to visuali...
Experimental data obtained from flow visualization by vortex tagging was used to verify the computat...
An experimental study is conducted to investigate the vortex developments over high angles of attack...
Complex vertical patterns form over the surface of an airfoil in an accelerating flow started from r...
The flow structure on the upper side of a delta wing is extremely complex. At moderate angle of atta...
A delta wing is subjected to both static and dynamic variations of, angle-of-attack; the vortices fr...
The transformation of flow structure on a delta wing of moderate sweep angle is investigated during ...
Proper control of unsteady separated flow developments over the lifting surfaces of an aircraft may ...
The structure of the leading-edge vortex from a delta wing at high angle of attack is addressed usin...
The dynamics and decay of a wake vortex system in close ground proximity is investigated in a tow ta...
The results of flow visualization by means of PIV method on airfoils with spoilers and high-lift fla...
The article presents an experimental and numerical study of vortex generation and shedding from a NA...
AbstractVisualization test is performed at the water channel of BUAA. The vortex core is visualized ...
The formation and development of leading-edge vortices, vortex breakdown, and three-dimensional sepa...
We present the visual analysis of a biologically inspired CFD simulation of the deformable flapping ...
An experimental system that generates and visualizes unsteady motions in air was employed to visuali...
Experimental data obtained from flow visualization by vortex tagging was used to verify the computat...
An experimental study is conducted to investigate the vortex developments over high angles of attack...
Complex vertical patterns form over the surface of an airfoil in an accelerating flow started from r...
The flow structure on the upper side of a delta wing is extremely complex. At moderate angle of atta...
A delta wing is subjected to both static and dynamic variations of, angle-of-attack; the vortices fr...
The transformation of flow structure on a delta wing of moderate sweep angle is investigated during ...
Proper control of unsteady separated flow developments over the lifting surfaces of an aircraft may ...
The structure of the leading-edge vortex from a delta wing at high angle of attack is addressed usin...
The dynamics and decay of a wake vortex system in close ground proximity is investigated in a tow ta...
The results of flow visualization by means of PIV method on airfoils with spoilers and high-lift fla...
The article presents an experimental and numerical study of vortex generation and shedding from a NA...
AbstractVisualization test is performed at the water channel of BUAA. The vortex core is visualized ...
The formation and development of leading-edge vortices, vortex breakdown, and three-dimensional sepa...
We present the visual analysis of a biologically inspired CFD simulation of the deformable flapping ...