Control of vortex shedding from a cylinder at different sweep back angles

L. Taubert, I. Wygnanski

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Scopus citations

Abstract

The control of vortex shedding from a yawed cylinder at different sweep back angles 0°, 45° and 60°, is currently investigated at the University of Arizona. Active flow control is applied on the cylinder in the form of oscillatory, zero mass flux excitation through two slots located symmetrically on the circumference. Surface and wake pressure measurements are carried out, as well as application of flow visualization and Particle Image Velocimetry.

Original languageEnglish (US)
Title of host publication2nd AIAA Flow Control Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Print)9781624100307
DOIs
StatePublished - 2004
Event2nd AIAA Flow Control Conference 2004 - Portland, OR, United States
Duration: Jun 28 2004Jul 1 2004

Publication series

Name2nd AIAA Flow Control Conference

Other

Other2nd AIAA Flow Control Conference 2004
CountryUnited States
CityPortland, OR
Period6/28/047/1/04

ASJC Scopus subject areas

  • Fluid Flow and Transfer Processes
  • Aerospace Engineering
  • Control and Systems Engineering

Fingerprint Dive into the research topics of 'Control of vortex shedding from a cylinder at different sweep back angles'. Together they form a unique fingerprint.

  • Cite this

    Taubert, L., & Wygnanski, I. (2004). Control of vortex shedding from a cylinder at different sweep back angles. In 2nd AIAA Flow Control Conference (2nd AIAA Flow Control Conference). American Institute of Aeronautics and Astronautics Inc.. https://doi.org/10.2514/6.2004-2511