Title of article
Low-frequency unsteadiness of vortex wakes over slender bodies at high angle of attack
Author/Authors
Ma، نويسنده , , Baofeng and Huang، نويسنده , , Yu and Liu، نويسنده , , Tongxin، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2014
Pages
9
From page
772
To page
780
Abstract
A type of flow unsteadiness with low frequencies and large amplitude was investigated experimentally for vortex wakes around an ogive-tangent cylinder. The experiments were carried out at angles of attack of 60–80° and subcritical Reynolds numbers of 0.6–1.8 × 105. The reduced frequencies of the unsteadiness are between 0.038 and 0.072, much less than the frequency of Karman vortex shedding. The unsteady flow induces large fluctuations of sectional side forces. The results of pressure measurements and particle image velocimetry indicate that the flow unsteadiness comes from periodic oscillation of the vortex wakes over the slender body. The time-averaged vortex patterns over the slender body are asymmetric, whose orientation is dependent on azimuthal locations of tip perturbations. Therefore, the vortex oscillation is a type of unsteady oscillation around a time-averaged asymmetric vortex structure.
Keywords
EXPERIMENTS , fluid dynamics , Unsteady flow , Aerodynamics , vortex flow
Journal title
Chinese Journal of Aeronautics
Serial Year
2014
Journal title
Chinese Journal of Aeronautics
Record number
2265536
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